Changeset 133 for Publications/Wilfried Dron
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Publications/Wilfried Dron/JOURNAL - Scheduling Method for Network Lifetime Estimation of WSN/Scheduling Method for Network Lifetime Estimation of Wireless Sensor Network.tex
r132 r133 388 388 % correct bad hyphenation here 389 389 \hyphenation{op-tical net-works semi-conduc-tor} 390 390 \usepackage{cite} 391 \usepackage{graphicx} 392 \usepackage{graphicx} 393 \usepackage{xcolor} 394 \usepackage{upquote} 395 %\usepackage{hyperref} 396 \usepackage{url} 397 \usepackage{arydshln} 398 \usepackage{listings} 399 \usepackage{subfigure} 400 \usepackage{balance} 401 \usepackage{xspace} 402 \newcommand{\pmsg}{{\textit{PowerMessage}}} 403 \newcommand{\imsg}{{\textit{InterfaceMessage}}} 404 \newcommand{\smsg}{{\textit{SignalMessage}}} 405 \newcommand{\dmsg}{{\textit{DigitalMessage}}} 406 \newcommand{\amsg}{{\textit{AnalogMessage}}} 407 \newcommand{\cmsg}{{\textit{ControlMessage}}} 408 \newcommand{\phymsg}{{\textit{PhysicalMessage}}} 409 \newcommand{\fm}{{{FM}}} 410 \newcommand{\pmm}{{{PM}}} 411 \newcommand{\phym}{{{PhyM}}} 412 413 \newcommand{\warn}{\textcolor{red}{\textbf{[REF]\space}}} 414 \newcommand{\tuple}[1]{\ensuremath{\left \langle #1 \right \rangle }} 415 \newcommand{\todo}[1]{\textcolor{blue}{{\bf Todo --\xspace}{\em #1}}} 416 \newcommand{\ie}{{\it i.e.},\xspace} 417 \newcommand{\eg}{{\it e.g.},\xspace} 418 \newcommand{\etal}{{\it et al.}\xspace} 419 \newcommand{\cf}{{\it c.f.},\xspace} 420 421 \newcommand{\sa}{{\textit{SA}}} 422 \newcommand{\fed}{{\textit{FED}}} 423 \newcommand{\sued}{{\textit{SUED}}} 424 \newcommand{\ffs}{{\textit{FFS}}} 391 425 392 426 \begin{document} … … 394 428 % paper title 395 429 % can use linebreaks \\ within to get better formatting as desired 396 \title{ Bare Demo of IEEEtran.cls for Journals}430 \title{Scheduling Methods for Network Lifetime Estimation of Wireless Sensor Networks} 397 431 % 398 432 % … … 406 440 % 407 441 408 \author{Michael~Shell,~\IEEEmembership{Member,~IEEE,} 409 John~Doe,~\IEEEmembership{Fellow,~OSA,} 410 and~Jane~Doe,~\IEEEmembership{Life~Fellow,~IEEE}% <-this % stops a space 411 \thanks{M. Shell is with the Department 412 of Electrical and Computer Engineering, Georgia Institute of Technology, Atlanta, 413 GA, 30332 USA e-mail: (see http://www.michaelshell.org/contact.html).}% <-this % stops a space 414 \thanks{J. Doe and J. Doe are with Anonymous University.}% <-this % stops a space 415 \thanks{Manuscript received April 19, 2005; revised January 11, 2007.}} 442 \author{Wilfried~Dron,~\IEEEmembership{Member,~IEEE,} 443 Khalil~Hachicha,~\IEEEmembership{Fellow,~OSA,} 444 and~Patrick~Garda,~\IEEEmembership{Life~Fellow,~IEEE}% <-this % stops a space 445 \thanks{W. Dron, K. Hachicha and P. Garda are with the UPMC Univ Paris 6, UMR 7606, Laboratoire d'Informatique de Paris 6. They are also with CNRS, UMR7606, LIP6. 446 F-75005, Paris, France; 447 e-mail: \texttt{[wilfried.dron; khalil.hachicha; patrick.garda]@lip6.fr}.}% <-this % stops a space 448 \thanks{Manuscript received Month Day, Year; revised Month Day, Year.}} 416 449 417 450 % note the % following the last \IEEEmembership and also \thanks - … … 436 469 437 470 % The paper headers 438 \markboth{Journal of \LaTeX\ Class Files,~Vol.~6, No.~1, January~2007}% 439 {Shell \MakeLowercase{\textit{et al.}}: Bare Demo of IEEEtran.cls for Journals} 471 \markboth{Transactions on COMPUTER-AIDED DESIGN of Integrated Circuits and Systems,~Vol.~X, No.~Y, Month~Year}% 472 {} 473 %{Shell \MakeLowercase{\textit{et al.}}: Bare Demo of IEEEtran.cls for Journals} 440 474 % The only time the second header will appear is for the odd numbered pages 441 475 % after the title page when using the twoside option. … … 469 503 \begin{abstract} 470 504 %\boldmath 471 The abstract goes here. 505 The network lifetime is a major constraint for the design of WSN's hardware and software. 506 %While several simulation tools are focused on power consumption estimation, the network lifetime has been estimated using an ideal battery model. 507 While several simulation tools are focused on estimating power consumption, the lifetime is commonly computed using a simple ideal battery model. 508 As a consequence, issues related with the use of a more realistic (non-ideal) battery model are not addressed yet. 509 Considering the error that is made in node's lifetime estimation using an ideal battery model (up to 40\%), specifications-based models have been implemented to achieve more reliable predictions. 510 In this context, we introduce four scheduling methods to address the challenges relative to such battery models. 511 These methods aim to manage energy transactions between the wireless node model and a non-ideal battery model. 512 %In this context, we introduce four scheduling methods to manage the energy transactions between the wireless node model and a non-ideal battery model, allowing a more accurate network lifetime estimation to be achieved. 513 Each of our methods is analyzed and compared through a typical temperature sensing application case. 514 We conducted several simulations considering power consumption estimation, simulation performances, node lifetime estimation and scalability. 515 Comparison of the obtained results highlights two methods, one more accurate but, rather slow, whereas the other is strongly scalable but less accurate. 472 516 \end{abstract} 473 % IEEEtran.cls defaults to using nonbold math in the Abstract.474 % This preserves the distinction between vectors and scalars. However,475 % if the journal you are submitting to favors bold math in the abstract,476 % then you can use LaTeX's standard command \boldmath at the very start477 % of the abstract to achieve this. Many IEEE journals frown on math478 % in the abstract anyway.479 517 480 518 % Note that keywords are not normally used for peerreview papers. 481 519 \begin{IEEEkeywords} 482 IEEEtran, journal, \LaTeX, paper, template.520 battery, lifetime estimation, wsn, OMNeT++, scheduling. 483 521 \end{IEEEkeywords} 484 522 … … 501 539 502 540 \section{Introduction} 503 % The very first letter is a 2 line initial drop letter followed 504 % by the rest of the first word in caps. 505 % 506 % form to use if the first word consists of a single letter: 507 % \IEEEPARstart{A}{demo} file is .... 508 % 509 % form to use if you need the single drop letter followed by 510 % normal text (unknown if ever used by IEEE): 511 % \IEEEPARstart{A}{}demo file is .... 512 % 513 % Some journals put the first two words in caps: 514 % \IEEEPARstart{T}{his demo} file is .... 515 % 516 % Here we have the typical use of a "T" for an initial drop letter 517 % and "HIS" in caps to complete the first word. 518 \IEEEPARstart{T}{his} demo file is intended to serve as a ``starter file'' 519 for IEEE journal papers produced under \LaTeX\ using 520 IEEEtran.cls version 1.7 and later. 521 % You must have at least 2 lines in the paragraph with the drop letter 522 % (should never be an issue) 523 I wish you the best of success. 524 525 \hfill mds 541 \IEEEPARstart{T}{he} network lifetime is a key parameter of the wireless sensor network characterization~\cite{lifetime}. 542 It reflects the time while the network can operate properly according to application-defined constraints. 543 %Even if almost every application defines its own constraints, the network lifetime cannot be estimated without being able to estimate the node's lifetime. 544 Even if almost every application defines its own constraints, the network lifetime is estimated using the individual node's lifetime information. 545 Since some specific application requires the nodes to have a long lifetime~\cite{outdoor_gplatform} (\eg from several weeks to several years) and/or the network to count several dozen of nodes~\cite{wsn_trends}, it is common to use simulation and modeling tools to design such devices. 546 547 Nodes are battery-powered, thus the power consumption of the node and its battery characteristics are both necessary to determine its lifetime. 548 The power consumption profile is easily accessible from hardware measurements~\cite{wsn_energy} whereas it is more challenging to extract battery characteristics. 549 Hence, it is common to use an ideal battery model to model the node's power source. 550 This model is known as a battery with a linear discharge curve and a fixed output voltage. 551 Far from the real battery behavior, this model has the advantage to be flexible enough to not address the physical and electrical laws that exist in a real system. %between a real battery and the node that it supplies. 552 %Nevertheless, when more accuracy is needed (as it is for medical applications for instance~\cite{wsn_app_medical_survey}) a more realistic battery model is required. 553 To obtain more accurate lifetime estimation, another battery model, closer to the real battery behavior, is required. 554 It can be either based on experimental measurements or technical specifications. 555 To remain consistent using such a model, electrical laws have to be applied. 556 Therefore, it is important to pay attention to the way power transactions between battery and supplied components are acheived. 557 In other words, the scheduling of the energy transactions trough the simulated time is crucial (\cf Fig.~\ref{archi_methods}). 558 %As a consequence, the scheduling of the energy transactions among the battery and the electronic components models is important. 559 %Actually, it has a strong impact over the node's lifetime prediction. 560 %In this article, we show that the way this scheduling is achieved impact significantly the lifetime estimation. 561 %Moreover, the way this scheduling is managed impacts the overall simulation performances and therefore, the ability to run large scale and/or long time simulation. 562 %As a side effect, the scheduling method also impact the overall simulation performances, restricting the ability to simulate large scale and/or long time lasting networks. 563 564 In this context, we introduce four scheduling methods to schedule the energy transactions in a modeled wireless sensor network node. 565 %We show that these methods are influencing the node lifetime estimation. 566 We show that the way this scheduling is achieved impact significantly the lifetime estimation showing difference in the obtained results that reaches 11.7\%. 567 %Moreover, the simulation's performance is also impacted, bounding the uses of certain methods to small-sized networks or short lifetime modeling. 568 As a side effect, the scheduling method also impacts the overall simulation performances, restricting the ability to simulate large scale and/or long time lasting networks. 569 This article is structured as follows. 570 The second section hold the background of this work. 571 The scheduling methods principles are explained in the section 3. 572 The fourth section address the implementation of these methods in OMNeT++ trough a WSN framework that is oriented toward power consumption estimation. 573 Finally, the two last sections hold respectively the simulation results and the discussion of these results. 574 575 \begin{figure} 576 \begin{center} 577 \includegraphics[scale=0.35]{architecture.pdf} 578 \caption{\label{archi_methods} 579 \textbf{Application example of the scheduling methods:} 580 Here, \textsl{scheduling} stands for the way the supply voltage (v) is transmitted from battery to components and the way the instantaneous current draw (i) is transmitted from the component to the battery through the simulated time. 581 } 582 \end{center} 583 \end{figure} 584 585 \section{Background} 586 The scheduling method for energy transactions have not been addressed yet, thus there is no previous work on that subject. 587 However, there are related works that are dealing with the power consumption estimation issues for the wireless sensor network simulation. 588 Since the node lifetime estimation relies on the battery models as well it is important to give a brief introduction to the battery behavior. 589 In that purpose, this section holds a short background about the battery behavior before addressing the core-related works. 590 591 \subsection{Battery Behavior and Modeling} \label{sect:battery_desc} 592 The batteries are electrochemical power sources. 593 In contrast with the wired power sources, the amount of energy that they carry is limited. 594 This amount of energy is called \textit{nominal capacity} if the battery is new or \textit{residual capacity} (shorten to \textit{residual}) if it has been partially used. 595 Considering a battery under use, its residual varies with the ambient temperature and the instantaneous current draw. 596 In other words, the available amount of energy change over the time according to the aforementioned factors. 597 The battery's \textit{nominal current} (set by the manufacturer) represent the ``normal operation'' current limit under continuous draw. 598 The term \textit{effective capacity} stands for the battery's capacity that is really available given a set of condition (\eg specific instantaneous current draw and a temperature). 599 Furthermore, their supply voltage varies as well with temperature and instantaneous current draw but also with the residual. 600 As a consequence, a specific current draw can produce a drift in the battery's supply voltage value. 601 According to the ohm law, this drift will change the current draw itself leading to a new drift. 602 %Considering a resistive circuit, the voltage value would reach an equilibrium which is not the case considering regulated system like voltage regulators for instance. 603 %All these assumptions were experimentally validated. 604 605 A first study highlights the fact that the way in which the components are drawing the current has a strong influence in the \textsl{effective capacity}~\cite{battery_char}. 606 These observations were confirmed by a more recent work that characterized commercial Li-Ion batteries behaviors through real measurements~\cite{battery_char_new}. 607 In this work, {K. Mikhaylov} and {J. Tervonen} observed again that the available capacity of the battery depends mainly on the instant current draw under constant temperature. 608 Another article that focuses on remaining capacity measurements agrees on the same conclusion~\cite{remaining_capacity_measurement}. 609 This last work addressed the specific case of determining the remaining battery capacity for a wireless sensor node using a method that consider the effective capacity and the instantaneous current draw instead of the voltage information. 610 611 More battery centered work were achieved to reach a better understanding of the battery properties. 612 Among them, another property known as \textit{relaxation effect} is explained in two articles written by L. Feeney and al.~\cite{battery_feeney,battery_model_feeney}. 613 As mentioned, when a strong current is drawn from the battery, its \textsl{effective capacity} decrease. 614 In other words, its actual available energy is lower than the nominal value. 615 This assumption is valid for a current draw that remains the same until the end of the battery life. 616 If, for instance, the current draw decrease to a value that is beyond the battery's ``nominal current'', the battery will ``recover'' some capacity. 617 618 To summarize, there are strong evidences that explain the limitations of ideal battery model. 619 While this model is extremely flexible and fast thanks to the fact that it is not dependent on any phenomena, it is highly inaccurate and does not reproduce the behavior of a real battery. 620 621 \subsection{Simulation and Modeling Environments} 622 There are several simulators and frameworks that enable the power consumption estimation. 623 Among them, a distinction is made between the environments that are oriented towards a specific platform and those that are more general, allowing any platform to be modeled. 624 TOSSIM~\cite{tossim_ws} is, for instance, a network simulator dedicated to Tiny-OS~\cite{tinyos}. 625 This simulator is extended by many further work. 626 The most noticeable are Power-TOSSIM~\cite{powertossim_ws} and mTOSSIM~\cite{mtossim}. 627 Power-TOSSIM enables the power consumption to be computed after the simulation ends. 628 In contrast, mTOSSIM go further allowing the lifetime to be estimated. 629 It does so using a super-capacitor to model the power supply of the nodes. 630 The super-capacitor behavior is very different from battery behavior (\cf Section~\ref{sect:battery_desc}). 631 As a consequence, this model cannot be used to estimate the lifetime of nodes equipped with batteries. 632 633 %Platform-dedicated simulation environment are for instance Cooja~\cite{cooja}, the simulator of ContikiOS or Power-Tossim~\cite{powertossim_ws}, the simulator of Tiny-OS. 634 %While these two simulators can achieve a precise power consumption estimation according to a specific application and its targeted hardware platform~\cite{powertossimz}, their main drawback is to be limited to the OS that they are simulating. 635 %Furthermore, none of them is providing a node lifetime estimation or only based on ideal battery model. 636 %As a consequence, these works are out of the scope of this paper. 526 637 527 \hfill January 11, 2007 528 529 \subsection{Subsection Heading Here} 530 Subsection text here. 531 532 % needed in second column of first page if using \IEEEpubid 533 %\IEEEpubidadjcol 534 535 \subsubsection{Subsubsection Heading Here} 536 Subsubsection text here. 537 538 539 % An example of a floating figure using the graphicx package. 540 % Note that \label must occur AFTER (or within) \caption. 541 % For figures, \caption should occur after the \includegraphics. 542 % Note that IEEEtran v1.7 and later has special internal code that 543 % is designed to preserve the operation of \label within \caption 544 % even when the captionsoff option is in effect. However, because 545 % of issues like this, it may be the safest practice to put all your 546 % \label just after \caption rather than within \caption{}. 547 % 548 % Reminder: the "draftcls" or "draftclsnofoot", not "draft", class 549 % option should be used if it is desired that the figures are to be 550 % displayed while in draft mode. 551 % 552 %\begin{figure}[!t] 638 Regarding the more general simulation environments, there are several network simulators like NS-2/3~\cite{ns2_ws}, OMNeT++~\cite{omnet_ws}, WSNeT~\cite{wsnet} or IdeaOne~\cite{ideaone}. 639 Some of them are able to estimate power consumption thanks to extension called \textit{frameworks}. 640 However, the goal of these environments is to deal with network modeling issues more than network lifetime estimation. 641 The OMNeT++ simulator is less concerned than the other environments since its flexibility allows new features to be integrated more easily as described in many surveys \cite{sim_survey_0,sim_survey_1,sim_survey_2,sim_survey_3} or in dedicated report from A. Varga and R. Hornig~\cite{omnet_overview}. 642 As a consequence, several~\textit{power-aware} framework were developed over the previous years. 643 Energy Model~\cite{modeling_energy}, Pawis~\cite{pawis_fm_2} and Energy Framework~\cite{energy_fm} were thus introduced. 644 Unfortunately a common short-coming of these framework is that none of them provides a non-ideal battery model. 645 646 Nevertheless, this short-coming was partially covered in an extension of the Energy Framework. 647 In their article, K. Mikhaylov and J. Tervonen were presenting a battery model~\cite{energy_fm_2} that was validated through measurement of real battery. 648 Unfortunately, this validation does not consider battery supply voltage variations due to the current draw. 649 Furthermore, it neglects the internal resistance of the battery and the relaxation effect. 650 A side observation that the authors made is the fact that using an ideal battery model leads to an over-evaluation of the battery lifetime of almost $40$\%. 651 %Their first conclusion is the fact that using an ideal battery model leads to an over-evaluation of the battery lifetime of almost $40$\%. 652 %Unfortunately, the techniques that were used to schedule the transaction between the battery model and the components model were not presented. 653 %Moreover, the simulation case that was chosen was limited to a simple resistive model in which the supply voltage drifts were not considered. 654 %As a result, it is difficult to re-use this work as a base for the network lifetime estimation. 655 A last power-aware framework for OMNeT++ was introduced~\cite{newcas}. 656 The battery model that is provided by the authors was build following technical specifications. 657 Finally, the conclusion of their work states on the fact that using of the event driven technique together with their battery model results in erroneous battery lifetime estimations. 658 To address this issue, they introduced a periodical scheduling method called \textit{Fixed Frequency Sampling} method. 659 660 %This latest framework was selected to implement the scheduling method because of its unique component oriented architecture and the several proposed models. 661 %The following section is dedicated to the description of the methods. 662 %Therefore, the firstly introduced scheduling method \textit{Fixed Frequency Sampling} will be exposed again in a more detailed way. 663 664 \section{Scheduling Methods} \label{sec:schedul_meth} 665 Our scheduling methods can be used in any structure that model one to N battery-supplied components. 666 Modeling of the supply voltage and the instantaneous current draw is the only requirement that could limit their application. 667 The architecture that is considered here is composed of one to N components model and a battery that supply them (\cf Fig.\ref{archi_methods}). 668 A concrete application case is added as example after the general descriptions. 669 % in order to expose the differences between every scheduling method. 670 Integration of these scheduling algorithms is explained as the conclusion of the section. 671 672 %%%%% METHODS DESCRIPTION 673 \begin{figure} 674 \begin{center} 675 \includegraphics[scale=0.45]{schedule_FFS.pdf} 676 \caption{\label{figure1} 677 \textbf{Fixed frequency sampling method states graphic:} 678 This graph shows the principle of the \ffs\xspace method. 679 It appears that the battery update are triggered periodically (each \textit{T} second) after the step~5. 680 } 681 \end{center} 682 \end{figure} 683 684 \subsection{Fixed Frequency Sampling method (FFS)} 685 The \textit{Fixed Frequency Sampling} method (shorten to \ffs) was introduced into prior work~\cite{newcas}. 686 This method relies on a periodic update of the battery's parameters and the current drawn by the components. 687 Figure~\ref{figure1} is a state chart that describe its algorithm. 688 First of all, the battery initiates the simulation by sending its supply voltage value to the component. 689 This allow the components to turn into ON mode. 690 Then, they sends back their averaged instantaneous current consumption over the previous period (which is null for the very first period). 691 The battery residual and the supply voltage are then updated according to the received current draw value. 692 Finally, if there is enough energy in the battery, the next update is scheduled at $t+T$ time (\textit{T} being the ``sampling period'' expressed in second). 693 If the battery is depleted, it sends a $0.0$V supply voltage that turns the components into OFF mode. 694 695 \subsection{Self Updating Event Driven method (SUED)} 696 In contrast with the \ffs\xspace method, the \textit{Self Updating Event Driven} method takes into account every current draw changes instantaneously. 697 The \sued\xspace scheduling method uses the same state chart as the \ffs\xspace method (\cf Fig.\ref{figure1}) except that it triggers additional battery updates as explained in the following. 698 When the simulation starts, the battery sends its supply voltage value to the components. 699 The components send back their instantaneous current draw. 700 Then the supply voltage and the remaining capacity of the battery are updated using the received value of the current draw. 701 This current draw value is stored. 702 If none of the components change their instantaneous current draw value, the battery will be updated every \textit{T} seconds. 703 When a component changes its power mode (\eg ON $\rightarrow$ POWER DOWN), the corresponding instantaneous current draw value is sent to the battery. 704 Then, the regular updating process is interrupted. 705 The battery residual and the supply voltage are updated for the time elapsed from the last battery's update using the latest stored current draw value. 706 Finally, the just received instantaneous current draw value is stored and the regular updating process starts again by scheduling the next update at $t+T$. 707 708 \begin{figure} 709 \begin{center} 710 \includegraphics[scale=0.45]{schedule_FED.pdf} 711 \caption{\label{figure3} 712 \textbf{Fast event driven method state graphic:} 713 This graph shows the principle of the \fed\xspace method. 714 In this method, the battery update are triggered by each changes in the operating state of the components. 715 } 716 \end{center} 717 \end{figure} 718 719 \subsection{Fast Event Driven method (FED)} 720 The \textit{Fast Event Driven} method is derived from the ``formal'' event driven simulation technique. 721 As a consequence, the battery updates are triggered by each current draw changes. 722 The sate chart depicted Figure~\ref{figure3} represent the behavior of this scheduling method. 723 The battery initiates the simulation by sending its supply voltage value. 724 As a consequence, the components change their state from OFF to ON and send back their associated instantaneous current draw value. 725 Alike the \sued\xspace method, this value is stored in the battery model. 726 When the component changes its state again, this value will be updated. 727 Before storing the just received value, a battery update is processed. 728 %Actually, it will estimate and check its new residual value considering the time elapsed from the previous update. 729 This update consist of checking and computing the new battery's residual considering the time elapsed from the previous update. 730 Battery's supply voltage value is also updated but using the new instantaneous current draw value and the residual that has just been estimated. 731 Finally, this supply voltage value is sent to the component. 732 733 Since the \fed\xspace scheduling method do not update the battery periodically, using this method can lead to node operating without energy. 734 If there is no event that makes the current draw change such as power mode changing, the simulation can run even if the battery is totally depleted at a certain point. 735 %As a consequence, another mechanism is required. 736 A way to avoid this issue is to ``plan'' the end of the battery life assuming that there will be no more event. 737 To be consistent, this end of life forecast has to be re-evaluated each time the current draw value changes. 738 In other words, the battery's end of life has to be re-planned each time that a battery update is triggered. 739 740 \subsection{Self Adaptive method (SA)} 741 The \textit{Self Adaptive} method is based on both a periodical update schedule and a event-driven like schedule. 742 %Actually, the previously introduced method are sensitive to the time and/or to the current draw changes events. 743 In addition, the \sa\xspace method is sensitive to the current draw value. 744 Battery behavior observations allow us to make the following assumption: The discharge curve can be separated in two areas, a pseudo-linear area (before the \textit{nominal current} value) and a non-linear area (after the \textit{nominal current} value). 745 The border between these two areas is the \textit{nominal current draw} (\cf Sec.~\ref{sect:battery_desc}). 746 As a consequence, the \sa\xspace scheduling method changes the way it triggers battery's and components updates according to the instantaneous current draw value. 747 When this value is under the \textit{nominal current} value of the modeled battery, the battery updates are triggered in the same way as if the \fed\xspace method were used. 748 In the opposite case (the current draw is under the \textit{nominal current} value), these updates are triggered as if the \ffs\xspace scheduling method were used. 749 750 On the one hand, this scheduling algorithm is able to enhance the accuracy of the estimation when it is necessary (when the battery model is strongly non-linear) and on the other hand, it is able to run the simulation faster when there is no need to (when the battery model is almost linear). 751 752 \subsection{Application example} 753 The chosen application example is a single component that is supplied by a battery. 754 The functional behavior of this component is not discussed here since the meaningful information is its current draw consumption. 755 As a consequence, the power mode states are the only information that are considered. 756 The following mode sequence was arbitrarily chosen: 757 \begin{itemize} 758 \item OFF $\rightarrow$ ON $\rightarrow$ POWER DOWN $\rightarrow$ ON. 759 \end{itemize} 760 The Figure~\ref{time} is a representation of each scheduling method applied to our example. 761 %Each of the four graphs illustrates the results of its method applied to the example case. 762 All the graph are time aligned making the difference between each scheduling method easier to understand. 763 764 \begin{figure} 765 \begin{center} 766 \includegraphics[scale=0.45]{method_global.pdf} 767 \caption{\label{time} 768 \textbf{Application example of the scheduling methods:} 769 This figure is a time graph that shows the application of each scheduling method to our application example. 770 The \ffs\xspace method trigger battery update according to its sampling period \textit{T}. 771 The \sued\xspace method trigger as well the update of the battery each \textit{T} seconds but also when a component changes its operating state. 772 The \fed\xspace method only triggers battery updates on the components change. 773 The \sa\xspace method use periodic update when precision is required and event driven updates when less precision is needed. 774 } 775 \end{center} 776 \end{figure} 777 778 Figure~\ref{time}a is the graph that represent the \ffs\xspace method application. 779 The updates of the battery and the component's current draw changes are asynchronous. 780 Moreover, the supply voltage updates are delayed by one period in comparison with the current draw updates. 781 In other words, the supply voltage value that is used by the component to compute its draw is the one that has been estimated the previous period by the battery model. 782 Figure~\ref{time}b represent the application of the \sued\xspace method. 783 In contrast with the \ffs\xspace method, it appears that the battery's updates are synchronized with the current draw changes. 784 The periodical update is also observable while the component is in LOW POWER mode. 785 Alike the \ffs\xspace method, the supply voltage updates are also delayed. 786 787 The application of the \fed\xspace method is plotted in the graph Figure~\ref{time}c. 788 %The fact that the battery updates happen only in synchronization with the component's power mode changes is highlighted. 789 The graph highlight that the battery updates happen only in synchronization with the component's power mode changes. 790 The Figure~\ref{time}d illustrates the application of the \sa\xspace method. 791 This method is sensitive to the current draw value in respect with the battery characteristics. 792 The current drawn in ON mode is assumed as being over the \textit{nominal current} value and the current drawn in the POWER DOWN mode is assumed as being under. 793 Consequently, periodical updates are achieved when the components is in ON mode whereas there is no update while the component is in LOW POWER mode. 794 795 %\section{Modeling and integration in the Framework} 796 \subsection{Framework Integration}\label{implementation} 797 As mentioned previously, we chose to implement our scheduling method in an OMNeT++ framework~\cite{newcas}. 798 %As mentioned previously, a power aware simulation environment was chosen to implement the scheduling methods \cite{newcas}. 799 %Actually, this environment is an OMNeT++'s framework that allows the wireless sensor node to be described with each of its electronic components. 800 This environment allows a node to be described with every of its electronic components. 801 Each component is described using two levels of description: a functional and a hardware one. 802 Practically, the components are described using a functional model and a power model. 803 Regarding the battery, a ``technical specification based'' model is provided. 804 805 The integration of our scheduling methods requires few modifications in the provided models. 806 Theoretically, each power model should be modified according to the chosen scheduling method. 807 Fortunately, the simulated architecture use a DC/DC step-down converter to keep the supply voltage between the battery and the components steady. 808 Therefore we consider the following assumption: the voltage do not change between the components' power model and the step down converter's output. 809 %WD: to moove in the discussion 810 %Actually, even if some precision can be lost by doing this, this assumption is realistic since the modeled converter is not used in its limitations. 811 Consequently to this assumption, the only models that requires to be modified are the battery model and the converter model. 812 813 To ensure reliable simulation results, mechanisms of the modified components were isolated into functions that takes every necessary information as parameters. 814 Even if it needed additional formalizing and coding efforts, this approach allows us to described the models independently from the scheduling method. 815 %The way and the sequence order in which the function are called determined the scheduling method. 816 817 \section{Modelling and simulation configuration} 818 \subsection{Battery Modelling} 819 The battery model that was used in the simulation is a model of the CR2032 battery from Panasonic~\cite{cr2032}. 820 The instantaneous current draw is considered to estimate the residual capacity and thus, predict the battery lifetime according to the technical specifications. %(cf. Fig.\ref{cr2032}). 821 %\begin{figure} 822 %\begin{center} 823 %\includegraphics[scale=1.1]{cr2032_capacity_vs_load_resistance.pdf} 824 %\caption{\label{cr2032}Panasonic CR2032: \textit{capacity vs. load resistance characteristic} \cite{cr2032} } 825 %\end{center} 826 %\end{figure} 827 The impact of the temperature variation on the battery were not considered in the following simulation case. 828 As a consequence, the battery's \textit{effective capacity} varies only with the instantaneous current draw. 829 \begin{figure} 830 \begin{center} 831 \includegraphics[scale=0.40]{eq_current_plot.pdf} 832 \caption{\label{eq_current} 833 \textbf{Equivalent and instantaneous current draw estimations:} 834 This graph show the difference between the instantaneous current drawn by the components (shorten to \textit{Inst.}, \cf $i(t)$ in Eq.~\ref{ieq}) and the current that is actually seen by the battery (shorten to \textit{Eq.}, \cf $i_{eq}$ in Eq.~\ref{ieq}). 835 } 836 \end{center} 837 \end{figure} 838 839 In this model, the capacity of the battery is considered as fixed. 840 Therefore, to model the impact of the instantaneous current draw on the \textit{relative capacity}, the equivalent current draw $i_{eq}(t)$ was considered. 841 It has been defined using the following equation: 842 \begin{equation}\label{ieq} 843 i_{eq}(t) = \frac{C_{nominal}}{C_{relative}(i(t))} \times i(t) 844 \end{equation} 845 Where $C_{nominal}$ is the \textit{nominal capacity} and $C_{relative}$ is the \textit{relative capacity} (according to the instantaneous current draw), both expressed in mAh. 846 The $i(t)$ is the instantaneous current expressed in mA. 847 The factor between $C_{nominal}$ and $C_{relative}$ is called the \textit{overdraw factor}. 848 Therefore, the equivalent current draw is expressed as a function of the present instantaneous current draw as depicted in the chart Figure~\ref{eq_current}. 849 This graph was plotted using a current draw ramp directly plugged in the battery model. 850 This battery modeling technique has the advantage of modeling both the \textit{effective capacity} and the \textit{relaxation} effects as well. 851 %Even if this abstraction of the real battery behavior is not perfect, it has the advantage of modeling both the \textit{effective capacity} and the \textit{relaxation} effects as well. 852 853 The equation that is used to estimate the battery's residual $R$ at the $t+\Delta t$ instant is the following one: 854 \begin{equation} 855 R(t+\Delta t) = R(t) - i_{eq}(t) \times \frac{\Delta t}{3600} 856 \end{equation} 857 Where $R(t)$ is the previous residual value in mAh, $i_{eq}(t)$ is the \textit{equivalent current draw} (\cf Eq.\ref{ieq}) in mA, $\Delta t$ the time while the $i_{eq}$ current was drawn expressed in second. 858 Finally, the $3600$ value stands for the conversion of $\Delta t$ in hours. 859 860 %\section{Simulation} 861 \subsection{Simulated Architecture} 862 The platform used as modeling base was a prototype under development. 863 It is composed of a NTC temperature sensor, a Texas Instruments (TI) MSP430FR5739 micro-controller~\cite{msp430_fr}, a TI CC2520 radio frequency transceiver~\cite{cc2520} and a TI TPS62122 step-down DC/DC converter~\cite{tps62122}. 864 The power supply is handled by 4 CR2032 batteries~\cite{cr2032} that are assembled in serial. 865 %The figure \ref{omnet} is a screen shot of the modelled node into the simulation environment. 866 %\begin{figure} 867 %\begin{center} 868 %\includegraphics[scale=0.55]{node_omnet.jpg} 869 %\caption{\label{omnet}Description of the node's architecture inside the WSN framework} 870 %\end{center} 871 %\end{figure} 872 The measurements that were used to build the MCU and the transceiver models are reported in Table~\ref{msp_meas}. 873 These measurements were made using a NI PXI-4071 ampere-meter integrated in a NI PXIe-1075 rack from National Instruments. 874 The used precision was seven and a half digits, the maximum precision of the device. 875 The measurements were achieved using a temperature regulated chamber from Binder. 876 The MCU firmware that was used to achieve this was the application that is embedded in the sensing node. 877 Consumption measurements of the MSP430 are not restricted to the core but include also the consumption of the whole chip. 878 879 \begin{table}[h] 880 \centering 881 \subtable[MSP430]{ 882 \begin{tabular}{|c||c|c|c|c|} 883 \hline 884 \textit{Mode} & Active & ADC+LPM4 & LPM4 \\ 885 \hline 886 Inst. current & 0.813mA & 0.326mA & 0.226mA \\ 887 \hline 888 \end{tabular} 889 } 890 %\begin{tabular}{cccccccc} 891 %& & & & & & &\\ 892 %\end{tabular} 893 \subtable[CC2520]{ 894 \begin{tabular}{|c||c|c|c|c|c|c|} 895 \hline 896 \textit{Mode} & XOSC Off & Idle & RX & RX LP & TX-18dBm \\ 897 \hline 898 Inst. current & 0.178mA & 1.776mA & 22.48mA & 18.79mA & 16.63mA\\ 899 \hline 900 \end{tabular} 901 } 902 \smallskip 903 \caption{\label{msp_meas}{\bf Experimental measurements of the current draw}} 904 \end{table} 905 906 Regarding the functional behavior, the application that is modeled is a typical temperature measuring scenario. 907 The network is organized in a star topology and the IEEE 802.15.4 protocol is used by the node to communicate. 908 The sensing node behavior is the following: 909 \begin{enumerate} 910 \item The node start to listen the channel to seek for a broadcast frame that comes from the central node; 911 \item Once it received the frame with the same PAN-ID and the expected source address, it acknowledge the subscription; 912 \item Every second it wakes up, takes a measure of the temperature and send it to the central node before going back to sleep. 913 \end{enumerate} 914 Each sensor has a time slot that is computed according to its own address, at the beginning of the run. 915 The central node is periodically broadcasting its subscription frame an turns into reception mode right after. 916 Therefore, its power consumption is high in comparison with the sensor node. 917 In the simulation, it is considered as being supplied by an ideal power source with infinite energy. 918 919 \section{Results} 920 All along this section, several simulation cases and their results are presented. 921 The sampling period \textit{T} of the \ffs, the \sued\xspace and the \sa\xspace (\cf Sect.~\ref{sec:schedul_meth}) scheduling methods were set to the same value ($50$us). 922 This choice is motivated by the simulation performances (\cf Sect.~\ref{sim_perfs}). 923 The computer that was used to obtain the results is based on a Core i7 860 @ 2.80GHz processor from Intel and 8 gigabytes of RAM. 924 Ubuntu LTS 12.04 was used as operating system. 925 The OMNeT++ version was the 4.3. 926 Simulator was configured to use only one core over eight in order to have no hardware acceleration that could biased the performance results. 927 %Each simulation case was run at least 10 times in order to verify the reliability of the obtained results. 928 929 \subsection{Power consumption estimation} 930 The power consumption estimation results were obtained by simulating four instances of the same node for one hour of simulated time. 931 Each node implements a different method to schedule the power transaction between the batteries and the components. 932 As a reference, another simulation was run within the same conditions but using ideal battery models instead of CR2032 models. 933 The battery's residual value results for both simulations are presented in Table~\ref{residual_results}. 934 935 \begin{table}[h] 936 \centering 937 \subtable[Ideal battery model, \textit{T}=50us]{ 938 \begin{tabular}{|c||c|c|c|c|} 939 \hline 940 & FFS & SUED & FED & SA\\ 941 %\hline 942 %\multicolumn{5}{|c|}{Nodes with Ideal model (\textit{T}=50us)} \\ 943 \hline 944 Residual (mAh)&$\textbf{219.9273}$&$\textbf{219.9273}$&$\textbf{219.9273}$&$\textbf{219.9273}$\\ 945 %Consumed Cap. (mAh)&$0.0727$&$0.0727$&$0.0727$&$0.0727$\\ 946 Av. $i_{eq}(t)$ (uA)&$72.7$&$72.7$&$72.7$&$72.7$\\ 947 %Av. voltage (V)&$12.00$&$12.00$&$12.00$&$12.00$\\ 948 \hline 949 \end{tabular} 950 } 951 \subtable[CR2032 battery model, \textit{T}=50us]{ 952 \begin{tabular}{|c||c|c|c|c|} 953 \hline 954 & FFS & SUED & FED & SA\\ 955 %\hline 956 %\multicolumn{5}{|c|}{Nodes with CR2032 model (\textit{T}=50us)} \\ 957 \hline 958 Residual (mAh)&$\textbf{219.9249}$&$\textbf{219.9248}$&$\textbf{219.9167}$&$\textbf{219.9137}$\\ 959 %Consumed Cap. (mAh)& $0.0751$& $0.0752$& $0.0833$& $0.0863$\\ 960 Av. $i_{eq}(t)$ (uA)& $75.1$& $75.2$& $83.3$& $86.3$\\ 961 \hline 962 \end{tabular} 963 } 964 \smallskip 965 \caption{\label{residual_results} 966 {\bf Battery's residual estimation results:} 967 {\textnormal{ 968 The battery residual estimation and the average equivalent current ($i_{eq}(t)$, \cf Eq.~\ref{ieq}) do not change for the ideal battery model regardless of the scheduling method. 969 In contrast, they are different for each scheduling method using the technical specification based battery model} 970 } 971 } 972 \end{table} 973 974 %\begin{table}[h] 553 975 %\centering 554 %\includegraphics[width=2.5in]{myfigure} 555 % where an .eps filename suffix will be assumed under latex, 556 % and a .pdf suffix will be assumed for pdflatex; or what has been declared 557 % via \DeclareGraphicsExtensions. 558 %\caption{Simulation Results} 559 %\label{fig_sim} 560 %\end{figure} 561 562 % Note that IEEE typically puts floats only at the top, even when this 563 % results in a large percentage of a column being occupied by floats. 564 565 566 % An example of a double column floating figure using two subfigures. 567 % (The subfig.sty package must be loaded for this to work.) 568 % The subfigure \label commands are set within each subfloat command, the 569 % \label for the overall figure must come after \caption. 570 % \hfil must be used as a separator to get equal spacing. 571 % The subfigure.sty package works much the same way, except \subfigure is 572 % used instead of \subfloat. 573 % 574 %\begin{figure*}[!t] 575 %\centerline{\subfloat[Case I]\includegraphics[width=2.5in]{subfigcase1}% 576 %\label{fig_first_case}} 577 %\hfil 578 %\subfloat[Case II]{\includegraphics[width=2.5in]{subfigcase2}% 579 %\label{fig_second_case}}} 580 %\caption{Simulation results} 581 %\label{fig_sim} 582 %\end{figure*} 583 % 584 % Note that often IEEE papers with subfigures do not employ subfigure 585 % captions (using the optional argument to \subfloat), but instead will 586 % reference/describe all of them (a), (b), etc., within the main caption. 587 588 589 % An example of a floating table. Note that, for IEEE style tables, the 590 % \caption command should come BEFORE the table. Table text will default to 591 % \footnotesize as IEEE normally uses this smaller font for tables. 592 % The \label must come after \caption as always. 593 % 594 %\begin{table}[!t] 595 %% increase table row spacing, adjust to taste 596 %\renewcommand{\arraystretch}{1.3} 597 % if using array.sty, it might be a good idea to tweak the value of 598 % \extrarowheight as needed to properly center the text within the cells 599 %\caption{An Example of a Table} 600 %\label{table_example} 601 %\centering 602 %% Some packages, such as MDW tools, offer better commands for making tables 603 %% than the plain LaTeX2e tabular which is used here. 604 %\begin{tabular}{|c||c|} 976 %\caption{\label{consumption_result}Power consumption estimation} 977 %\begin{tabular}{|c||c|c|c|c|} 605 978 %\hline 606 % One & Two\\979 %\multicolumn{5}{|c|}{Simulated time = 60 minutes} \\ 607 980 %\hline 608 %Three & Four\\ 981 % & FFS & SUED & FED & SA\\ 982 %\hline 983 %\hline 984 %\multicolumn{5}{|c|}{Power Consumption: Ideal model} \\ 985 %\hline 986 %Residual (mAh) & $\textbf{219.9273}$ & $\textbf{219.9273}$ & $\textbf{219.9273}$ & $\textbf{219.9273}$\\ 987 %Consumed C. (mAh) &$0.0727$&$0.0727$&$0.0727$& $0.0727$\\ 988 %Av. eq. current (uA) &$72.7$&$72.7$&$72.7$&$72.7$\\ 989 %Av. voltage (V)&$12.00$&$12.00$&$12.00$&$12.00$\\ 990 %\hline 991 %\hline 992 %\multicolumn{5}{|c|}{Power Consumption: CR2032 model} \\ 993 %\hline 994 %Residual (mAh) & $\textbf{219.9249}$& $\textbf{219.9248}$ & $\textbf{219.9167}$& $\textbf{219.9137}$\\ 995 %Consumed Energy (mAh) & $0.0751$& $0.0752$& $0.0833$& $0.0863$\\ 996 %\hline 997 %Max current (mA) & $3.99$ & $3.99$& $3.92$& $3.99$\\ 998 %Min current (mA) & $0.073$ & $0.073$& $0.071$& $0.071$\\ 999 %\hline 1000 %Max eq. current (mA) & $7.359$& $7.359$& $7.033$& $7.359$\\ 1001 %Min eq. current (mA) & $0.70$& $0.073$& $0.071$& $0.071$\\ 1002 %Av. eq. current (uA) & $75.1$& $75.2$& $83.3$& $86.3$\\ 1003 %\hline 1004 %Max voltage (V) & $12.0$& $12.0$& $12.0$& $12.0$\\ 1005 %Min voltage (V) & $9.98$& $9.98$& $10.67$& $9.98$\\ 1006 %Av. voltage (V) & $10.62$& $10.54$& $11.40$& $10.70$\\ 609 1007 %\hline 610 1008 %\end{tabular} 611 1009 %\end{table} 612 1010 613 614 % Note that IEEE does not put floats in the very first column - or typically 615 % anywhere on the first page for that matter. Also, in-text middle ("here") 616 % positioning is not used. Most IEEE journals use top floats exclusively. 617 % Note that, LaTeX2e, unlike IEEE journals, places footnotes above bottom 618 % floats. This can be corrected via the \fnbelowfloat command of the 619 % stfloats package. 620 621 1011 The first important observation is the fact that scheduling method do not influence the lifetime estimation in the case of ideal battery modeling (\cf Tab.~\ref{residual_results}(a)). 1012 Actually, the four nodes reach the end of the simulation with the same residual value ($219.9273$ mAh), the same current draw and the same voltage value. 1013 In contrast, the results obtained by the node that were equipped with CR2032 models are not equal (\cf Tab.~\ref{residual_results}(b)). 1014 These variations in the power consumption estimations highlight the fact that scheduling method do influence the residual estimation. 1015 Consequently, the node lifetime estimation is also influenced even if each battery model and each component model is the same. 1016 1017 \begin{table}[h] 1018 \begin{center} 1019 \begin{tabular}{|c||c|c|c|c|} 1020 \hline 1021 & FFS & SUED & FED & SA\\ 1022 \hline 1023 Max $i(t)$ (mA) & $3.99$ & $3.99$& $3.92$& $3.99$\\ 1024 Min $i(t)$ (mA) & $0.073$ & $0.073$& $0.071$& $0.071$\\ 1025 \hline 1026 Max $i_{eq}(t)$ (mA) & $7.359$& $7.359$& $7.033$& $7.359$\\ 1027 Min $i_{eq}(t)$ (mA) & $0.70$& $0.073$& $0.071$& $0.071$\\ 1028 %\hline 1029 %Av. eq. current (uA) & $75.1$& $75.2$& $83.3$& $86.3$\\ 1030 \hline 1031 \end{tabular} 1032 \end{center} 1033 \smallskip 1034 \caption{\label{current_results}{\bf Instantaneous $i(t)$ and equivalent current $i_{eq}(t)$ draw estimation (cf., Eq.~\ref{ieq}):} \textnormal{The estimated values are slightly different for each scheduling method.}} 1035 \end{table} 1036 1037 Focusing on the detailed results, the residual estimation that is obtained using the \ffs\xspace method is the highest one with $219.9429$ mAh. 1038 Firstly, the current draw is integrated over the \textit{T} period. 1039 This is comparable to a \textit{low pass filter} that cuts the edges of the current draw spikes. 1040 Secondly, the supply voltage value is the one that has been computed using the previous current draw value. 1041 The impact of the voltage drifts are consequently lowered. 1042 The \sued\xspace method suffers from the same observations, except for the spike transition thanks to the synchronized current updates. 1043 This explains why the average \textit{equivalent current draw} (\cf Eq.~\ref{ieq}) value that is obtained using the \sued\xspace scheduling method is slightly more important than the \ffs\xspace one ($75.2$uA $>$ $75.1$uA). 1044 To achieve better results with these scheduling methods, the Shannon theorem should be observed. 1045 In other word, the sampling period should be at least twice short as the shorter power mode changing of the system. 1046 In the present case, the shorter period is around 5us. 1047 Therefore a 2.5us period is the minimum period length regarding the accuracy and the precision of the estimation. 1048 Unfortunately, using such a small period results in an extremely slow simulation as presented in the next section. 1049 1050 %Another fact that could explain that the result of the sampling based method are not the same as the \fex\xspace and \sa\xspace methods is the numeric precision. 1051 Another noticeable result is the difference in the residual estimated with \ffs\xspace and \sued\xspace methods in comparison with \fed\xspace and \sa\xspace methods. 1052 These variations could be explained by the numeric precision. 1053 Since there is more computation using the CR2032 model than the ideal battery model, precision could have been lost in every intermediary value computation ending to a under-estimated power consumption. 1054 Actually, this phenomena is partially observable considering the current draw and the equivalent current draw estimation (\cf Tab.~\ref{current_results}). 1055 1056 \begin{table}[h] 1057 \centering 1058 \begin{tabular}{|c||c|c|c|c|} 1059 \hline 1060 & FFS & SUED & FED & SA\\ 1061 \hline 1062 Max voltage (V) & $12.0$& $12.0$& $12.0$& $12.0$\\ 1063 Min voltage (V) & $9.98$& $9.98$& $10.67$& $9.98$\\ 1064 %Av. voltage (V) & $10.62$& $10.54$& $11.40$& $10.70$\\ 1065 \hline 1066 \end{tabular} 1067 \smallskip 1068 \caption{\label{voltage_results} 1069 {{\bf Battery supply voltage estimation:} 1070 \textnormal{The estimated supply voltage values are the same except for the FED method.} 1071 } 1072 } 1073 \end{table} 1074 1075 Focusing on the event-driven based scheduling method \fed, the obtained residual estimation is lower than the \ffs\xspace and the \sued\xspace method but higher than the \sa\xspace method. 1076 This is a result of the event driven-like algorithm. 1077 The current drawn by the components is updated immediately when one of them changes its power mode. 1078 Once a new current value draw has been transmitted to the battery, its residual is computed and its voltage value is updated but there is no further updates from both the components and the battery until a components change its current draw again. 1079 This explain also why the average equivalent current obtained thanks to the \sa\xspace method was higher with $86.3$uA (\cf Tab.~\ref{residual_results}). 1080 The observation of the current draw and the equivalent current draw in the Table~\ref{current_results} are confirming this assumption. 1081 Actually, even if every battery has to supply the same current both the maximal current and the maximal equivalent current estimated using the \fed\xspace method are lower than the other methods. 1082 1083 The sampling mechanism of the \sa\xspace method allows the battery model to react almost instantly to every current draw variation. 1084 Finally, while the average voltage obtained using the \ffs\xspace, \sued\xspace and \sa\xspace methods are quite close, the supply voltage value obtained using the \fed\xspace method is higher (\cf Tab.~\ref{voltage_results}). 1085 This highlights once again the fact that updates are driven by the components' power state changes. 1086 1087 \subsection{Simulation performance} \label{sim_perfs} 1088 The simulation performance results were obtained by running the nodes for five minutes of CPU time (300 seconds). 1089 Two series of simulation were conducted. 1090 The first one consist of running one single node and its base station at a time. 1091 Each scheduling method is therefore evaluated on its own. 1092 The second one consist of the same principle but running a network of five identical nodes. 1093 The main results are presented in Table~\ref{residual_results}. 1094 In this table there is several abbreviation: 1095 \begin{itemize} 1096 \item the simulated time: \textit{\textbf{Sim.time}} 1097 \item the average simulated sec. per sec. ratio: \textit{\textbf{Av.Sim.s/s}} 1098 \item the number of simulated events: \textit{\textbf{N.ev.}} 1099 \item the average number of event per sec.: \textit{\textbf{Ev/s}} 1100 \end{itemize} 1101 1102 1103 The time indications give basic idea on how much of CPU time it would take if the simulation has to reach a specific time. 1104 The event indications give idea about the load of the simulation kernel. 1105 It allows to figure out the raw performances and eventually deduce the impact of porting the scheduling methods to another simulation environment. 1106 \begin{table}[h] 1107 \centering 1108 \begin{tabular}{|c||c|c|c|c|} 1109 \hline 1110 \multicolumn{5}{|c|}{CPU time = 5min (300 s)} \\ 1111 \hline 1112 & FFS & SUED & FED & SA\\ 1113 \hline 1114 \hline 1115 \multicolumn{5}{|c|}{1 Node} \\ 1116 \hline 1117 Av.Sim.s\slash s & \textbf{2.695} & \textbf{5.474} & \textbf{6699} & \textbf{3342}\\ 1118 \hline 1119 Sim.time & 13min:28s& 27min:22s & 23d:6h & 11d:22h\\ 1120 N.ev. &$48\times10^6$&$98\times10^6$&$80\times10^6$&$82\times10^6$ \\ 1121 Ev\slash s &$1.6\times10^5$&$3.2\times10^5$&$2.7\times10^5$&$2.7\times10^5$ \\ 1122 \hline 1123 \multicolumn{5}{|c|}{5 Nodes} \\ 1124 \hline 1125 Av.Sim.s\slash s & \textbf{0.576} & \textbf{1.218} & \textbf{1330} & \textbf{713.5}\\ 1126 \hline 1127 Sim.time & {2min:52s}&{6min:5s}& {4d:14h}& {2d:11h}\\ 1128 N.ev. &$51.8\times10^6$&$109.6\times10^6$&$86.6\times10^6$&$89.3\times10^6$ \\ 1129 Ev\slash s &$1.7\times10^5$&$3.6\times10^5$&$2.8\times10^5$&$2.9\times10^5$ \\ 1130 \hline 1131 \end{tabular} 1132 \smallskip 1133 \caption{\label{perf_table} 1134 {{\bf Simulation performance (\textit{T}=50us)}: 1135 \textnormal{This table summarize the performances of each method. The FFS and SUED scheduling methods are the slowest and the less scalable methods. In contrast, the FED and the SA scheduling methods allow to simulate in a faster way larger networks} 1136 } 1137 } 1138 \end{table} 1139 1140 Regarding the simulated time for a single node, the results are quite clear. 1141 The \ffs\xspace and the \sued\xspace method reach $13$ and $27$ minutes respectively. 1142 In contrast, the \sa\xspace method is able to simulate almost $12$ days in $5$ minutes of CPU time. 1143 The \fed\xspace method outperforms by reaching $23$ days of simulated time and almost $2$h simulated per second. 1144 The results of the 5 nodes are following the same trends. 1145 The average simulated second per second rate of the \ffs\xspace method decrease to $0.57$ sim.s/s which is quite slow since its under the ``unity rate'' of $1$ sim.s/s. 1146 The \sued\xspace method is slightly faster with 1.2 sim.s/s rate that enables it to reach $6$ minutes of simulated time in $5$ minutes. 1147 Finally, the best performances were obtained using the \sa\xspace and the \fed\xspace method with respectively 2 days and 4 days of simulated time. 1148 1149 As a consequence, the \ffs\xspace and the \sued\xspace method are not considered in the following experiments. 1150 This choice is motivated by the fact that these two methods are not suitable for long-time simulation (several months) nor for networks that implies several nodes. 1151 1152 \subsection{Node lifetime estimation} 1153 The node lifetime estimation results were obtained by running one single node and the central node until the first voltage drops that makes the node reset. 1154 This scenario focuses on the real node lifetime as it has been defined in the beginning of this article. 1155 If, for any reason, there is a voltage drop that makes the node reset, there is high chances that it happens again and again until the complete depletion of the battery. 1156 Therefore the node can be considered as dead or not reliable enough from the point of view of the network. 1157 1158 As mentioned before, only the \fed\xspace and the \sa\xspace method were considered in this experiments. 1159 Making the same run with the \ffs\xspace method would have require approximately 1 month of continuous run. 1160 The theoretical lifetime $L_{TH}$ of the node obtained with an ideal battery model is around 4 months ($L_{TH} \approx 220\slash 0.0727 \approx$ 4.2 months). 1161 This estimation implicitly assumes that the battery is able to supply the node until its total depletion, which is not the case. 1162 The node lifetime estimation results are presented in the Table~\ref{sim_table_2}. 1163 First analysis of these results reveals that estimation obtained by the \fed\xspace and the \sa\xspace methods are significantly different. 1164 The \fed\xspace node lasted three months and twelve days while the \sa\xspace node lasted three months and one day. 1165 This represent a difference of $11.7$\% between the two methods and a difference of $20.8$\% (\fed) and $35.0$\% (\sa) between each method's lifetime estimation and $L_{TH}$. 1166 1167 \begin{table}[h] 1168 \centering 1169 \begin{tabular}{|c||c|c|} 1170 \hline 1171 & FED & SA\\ 1172 \hline 1173 \hline 1174 \multicolumn{3}{|c|}{Node lifetime (\textit{T}=50us)} \\ 1175 \hline 1176 Lifetime & 3m:12d:7h:29min:0s & 3m:1d:8h:50min:29s\\ 1177 \hline 1178 Residual (mAh) & $0.0176$ & $\textbf{16.8062}$\\ 1179 \hline 1180 Simulation time & 22min:25s & 38min:18s\\ 1181 Av.Sim.s\slash s & $6700$ & $3510$\\. 1182 N.ev. &$3.6\times10^8$ &$64\times10^8$ \\ 1183 Ev\slash s &$2.7\times10^5$ & $2.8\times10^5$\\ 1184 \hline 1185 %Gain Factor & $98.5$ & $1.35$\\ 1186 %\hline 1187 \end{tabular} 1188 \smallskip 1189 \caption{\label{sim_table_2} 1190 {\bf Node lifetime estimation performance}: 1191 \textnormal{The difference of 11.7\% between the two methods highlight the fact that scheduling methods do influence the lifetime estimation.} 1192 } 1193 \end{table} 1194 1195 A closer observation of the residual values at the end of the simulation is highlighting the fact that the \sa\xspace node stops operate properly before the \fed\xspace node. 1196 It appears that the battery's voltages drift are not well modeled with the \fed\xspace method since the likelihood of the fact that the battery lasts until almost complete depletion ($0.0176$ mAh) is low. 1197 Considering the technical specification, the battery should not be able to handle the current spike of a RF frame transmission at this depletion level. 1198 Consequently, the results obtained by the \sa\xspace method are more realistic. 1199 Unfortunately, there is no means to measure the remaining capacity in a real battery to have a comparison point. 1200 Further experiments about battery discharge in this particular application case will be conducted in order to experimentally validate this hypothesis. 1201 1202 \subsection{Scalability} 1203 The last exposed experiment was conducted to evaluate the scalability of the \fed\xspace and the \sa\xspace scheduling methods. 1204 The simulated time was set to $24$h hours. 1205 Each simulation contained a complete network with $10$ to $250$ nodes and a central station. 1206 The obtained result are presented in the table \ref{sim_table_3}. 1207 1208 \begin{table}[h] 1209 \centering 1210 \begin{tabular}{|c||c|c|} 1211 \hline 1212 \multicolumn{3}{|c|}{Simulated time = 24h (\textit{T}=50us)}\\ 1213 \hline 1214 &FED&SA\\ 1215 \hline 1216 10 nodes & $2$min $11$s & $4$min $6$s \\ 1217 %\cdashline{2-3} 1218 50 nodes & $13$min $57$s & $24$min $3$s \\ 1219 %\cdashline{2-3} 1220 100 nodes & $36$min $17$s & $56$min $52$s\\ 1221 %\cdashline{2-3} 1222 250 nodes & $2$h $58$min & $3$h $45$min \\ 1223 \hline 1224 \end{tabular} 1225 \smallskip 1226 \caption{\label{sim_table_3} 1227 {\bf Scalability comparison: simulation time for 10 to 250 nodes}: 1228 \textnormal{This table is a comparison of the time that is required for each methods to reach 24h of simulated time considering various network size. The results show clearly that the SA method needs almost twice the time of the FED method to achieve it. However, when the size of the network increase, this factor decreases.} 1229 } 1230 \end{table} 1231 1232 First observation that can be made is the fact the evolution of the time as a function of the number of the nodes is not linear. 1233 Actually, simulating 250 nodes should be 25 times longer than simulating 10 nodes. 1234 Simulating 10 nodes with the \fed\xspace method takes 2.18 minutes but simulating 250 node takes almost three hours instead of 54 minutes as it could be expected. 1235 This is explained by the fact that each additional node adds a significant traffic load. 1236 A second observation is the fact that when network are small (\eg less than 50 nodes) the \fed\xspace method is roughly two time faster than the \sa\xspace method. 1237 This difference seems to decrease when the size of the network increase. 1238 With a 250 nodes network, using the \sa\xspace method takes only 26\% more time than the \fed\xspace method. 1239 1240 More generally, these results are highlighting the high scalability of the \fed\xspace method in comparison with the \sa\xspace method that is slower. 622 1241 623 1242 \section{Conclusion} 624 The conclusion goes here. 625 626 627 628 629 630 % if have a single appendix: 631 %\appendix[Proof of the Zonklar Equations] 632 % or 633 %\appendix % for no appendix heading 634 % do not use \section anymore after \appendix, only \section* 635 % is possibly needed 636 637 % use appendices with more than one appendix 638 % then use \section to start each appendix 639 % you must declare a \section before using any 640 % \subsection or using \label (\appendices by itself 641 % starts a section numbered zero.) 642 % 643 644 645 \appendices 646 \section{Proof of the First Zonklar Equation} 647 Appendix one text goes here. 648 649 % you can choose not to have a title for an appendix 650 % if you want by leaving the argument blank 651 \section{} 652 Appendix two text goes here. 653 1243 In this work, we have introduced four scheduling methods to address the specific issue of network lifetime estimation when a non-ideal battery model is used. 1244 Our first experiments revealed that the scheduling methods do have an impact on battery's lifetime estimations and thus on the node lifetime prediction. 1245 As expected, our results are showing that the sampling based methods are not suitable for large scale simulation whereas it seems to be the most intuitive way to reach an accurate and precise estimation. 1246 In contrast, event-driven based method is the fastest scheduling method whereas it appears to lead to inaccurate results. 1247 Finally, the compromise between the event-driven and the periodical scheduling methods was found as the \sa\xspace method which enables a fast and accurate network lifetime estimation. 1248 1249 Our future work will address the comparison of the lifetime prediction and the real measurement thanks to a WSN testbed oriented towards network lifetime characterization. 1250 The technical based proposed model will be compared to real measurement of the battery behavior. 1251 Finally, we will accentuate our efforts on the scheduling methods optimization with the goal of very-large scale and reliable network lifetime estimation. 654 1252 655 1253 % use section* for acknowledgement 656 1254 \section*{Acknowledgment} 657 658 659 The authors would like to thank... 1255 %Liam McNamara (SICS), Beshr Al Nahas (SICS). 660 1256 661 1257 … … 690 1286 % set second argument of \begin to the number of references 691 1287 % (used to reserve space for the reference number labels box) 692 \begin{thebibliography}{1} 693 694 \bibitem{IEEEhowto:kopka} 695 H.~Kopka and P.~W. Daly, \emph{A Guide to \LaTeX}, 3rd~ed.\hskip 1em plus 696 0.5em minus 0.4em\relax Harlow, England: Addison-Wesley, 1999. 697 698 \end{thebibliography} 1288 \bibliographystyle{IEEEtran} 1289 \bibliography{bib} 699 1290 700 1291 % biography section … … 709 1300 % or if you just want to reserve a space for a photo: 710 1301 711 \begin{IEEEbiography}{ Michael Shell}1302 \begin{IEEEbiography}{Wilfried Dron} 712 1303 Biography text here. 713 1304 \end{IEEEbiography} 714 1305 715 1306 % if you will not have a photo at all: 716 \begin{IEEEbiographynophoto}{ John Doe}1307 \begin{IEEEbiographynophoto}{Khalil Hachicha} 717 1308 Biography text here. 718 1309 \end{IEEEbiographynophoto} … … 722 1313 %\newpage 723 1314 724 \begin{IEEEbiographynophoto}{ Jane Doe}1315 \begin{IEEEbiographynophoto}{Patrick Garda} 725 1316 Biography text here. 726 1317 \end{IEEEbiographynophoto}
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