Kalman Filtering for Differential Drive Robots Tracking

Total Page:16

File Type:pdf, Size:1020Kb

Kalman Filtering for Differential Drive Robots Tracking XIII Simp´osio Brasileiro de Automa¸c˜ao Inteligente Porto Alegre – RS, 1o – 4 de Outubro de 2017 KALMAN FILTERING FOR DIFFERENTIAL DRIVE ROBOTS TRACKING Luis Aguiar∗, Marcos R. O. A. Maximo∗, Takashi Yoneyamay, Samuel Pinto∗ ∗Autonomous Computational Systems Lab (LAB-SCA), Computer Science Division, Aeronautics Institute of Technology Pra¸ca Marechal Eduardo Gomes, 50, Vila das Ac´acias, 12228-900 S~aoJos´edos Campos, SP, Brazil yElectronic Engineering Division, Aeronautics Institute of Technology Pra¸ca Marechal Eduardo Gomes, 50, Vila das Ac´acias, 12228-900 S~aoJos´edos Campos, SP, Brazil Emails: [email protected], [email protected], [email protected], [email protected] Abstract| This paper presents the application of the stochastic filtering techniques known as Extended Kalman Filter and Uscented Kalman Filter in the tracking and state estimation of differential drive robots. This work presents and describes these algorithms, the stochastic modeling for this specific problem, the results from implementation using real robot's data and performance evaluation from simulations. Keywords| Mobile Robots, Stochastic Filtering, Tracking 1 Introduction Tracking is a particularly important task con- cerning not only the VSS challenge but many Mobile robotics is a rich and growing field in mod- other applications. Finding the motion of an ob- ern technology. Recently, it has been achieving ject can be useful in navigation, video surveil- huge technical advancements and at the same time lance, satellite control, missile guidance etc. We finding several interesting applications from mili- have experienced a great progress in the proba- tary to domestic scenarios. A key element in the bilistic approach ()(S. Thrun and Fox, 2005) and robotics field is the movement tracking and the (Brookner, 1998)) using Bayesian filtering to deal state estimation of robot agents throughout the with tracking. Many problems can be cast into environment. As can be seen in some recent so- the problem of estimating the state of a dynamic phisticated robots, these tasks play an essential system from discrete noisy measurements. There- role in the development of advanced autonomous fore, the standard formulation includes the state machines. space and discrete-time approach (Arulampalam et al., 2001), using the world famous non-linear One particular class of mobile robots is the Gaussian filters (EKF and UKF) and the non- differential drive robots, which can be widely seen parametric Particle Filter. In addition to the po- in several applications due to its hardware sim- sition estimation, in several situations, it is also plicity and versatility. In this way, an interesting necessary to extract the velocity estimates from challenge involving these robots is the IEEE Very the measurement of the position alone. For exam- Small Size competition. VSS is a soccer based ple, one can mention some feedback control mod- challenge with autonomous robots with maximum els and trajectory planning algorithms which de- dimensions of 7:5cmx7:5cmx7:5cm. Each team mand an optimal velocity estimation. Some for- has three robots in the field and is allowed to have mulations of these bayesian filters aims to solve a camera fixed above it and also develop a vision this issue, as can be seen in (Palumbo et al., 2010) system. Most of the processing occur in a exter- and in (Bruno and Pavlov, 2004). nal computer which communicates with the agents using wireless interface. Therefore, the purpose of this paper is to This work is based on our recent efforts for the present the application of the Extended Kalman development of a tracking system for the ITAn- Filter, Uscented Kalman Filter and the linear droids' VSS team. ITAndroids is a robotics re- Kalman filter in the described VSS tracking prob- search group at Technological Institute of Aero- lem, as well as assessing its performance based on nautics which was refounded in mid-2011 after the Root Mean Square Error (RMSE) calculated some few years of inactivity. The group par- for several simulations and also applying it to real ticipates in several national and international data. In this work, Section 1 gives a presentation competitions. In particular, ITAndroids' VSS and an overview of the subject, Section 2 describes team has participated in the 2014 and 2015 edi- the mentioned techniques introducing the corre- tions of the Latin American Robotics Competi- spondent algorithms and Section 3 provides the tion (LARC) and Brazilian Robotics Competition stochastic model of the differential drive robots (CBR), which happen as one single event, achiev- in the tracking problem. Section 4 describes the ing the 4th place in the latest edition. procedure used in the covariance calibration pro- ISSN21758905 1520 XIII Simp´osio Brasileiro de Automa¸c˜ao Inteligente Porto Alegre – RS, 1o – 4 de Outubro de 2017 cess. Section 5 presents some implementation re- Extended Kalman Filter, in contrast with the lin- sults using the vision data from a real robot and ear one, may not be optimal and may produce un- also some simulation tests. Finally, in Section 6 desirable results for highly non-linear functions. we can see the main conclusions and final consid- For smooth non-linear functions, in which the erations. linearization gives a good local approximation of the function, the Extended Kalman Filter usu- 2 Probabilistic Localization ally has good performance. Equations (3) to (6) show precisely how the linearization is performed. In the state-space and discrete time approach to The complete EKF algorithm is presented in Al- the tracking problem, we represent the robot's gorithm 1. pose at time k 2 by its state vector x 2 n. Z k R @f (x; u ; w) From a probabilistic formulation, we define its F = k k−1 jw=0 (3) k x=xk−1jk−1 state as a vector of random variables, and for rep- @x resenting its state uncertainty we are interested in @fk(x; uk−1; w) w=0 Lk = j (4) the probability density function (pdf) of xk. @w x=xk−1jk−1 In order to use the concept of bayesian fil- @h (x; v) tering, two models are needed (Arulampalam H = k jv=0 (5) k x=xkjk−1 et al., 2001). A model describing the dynamic @x evolution of the state, called the movement model, @hk(x; v) v=0 Mk = j (6) represented in equation (1), and a second model @v x=xkjk−1 relating the noisy measurement to the state, called the measurement model, represented in equation Algorithm 1 EKF (2). Initialization x^0j0 = x^0 xk = f(xk−1; uk−1; wk−1) (1) P0j0 = P0 for k 1 to N do zk = h(xk; vk) (2) In equation (1), f is the propagation function, Prediction Step u is the vector of control commands and w is the k k x^kjk−1 fk(x^k−1jk−1; uk−1; 0) process associated random perturbations. Mean- @fk Fk jx=x^ while, in equation (2), h is the function that trans- @x k−1jk−1 L @fk j forms the state space into the observation space, k @w x=x^k−1jk−1 T T Pkjk−1 FkPk−1jk−1F + LkQkL with an associated random noise vk. We shall con- k k sider that wk and vk are independent and have Filtering Step null mean and covariance matrices Qk and Rk, @hk Hk jx=x^ respectively. The estimate of xk will be denoted @x kjk−1 @hk by x^kjk and its covariance matrix by Pkjk. Mk @v jx=x^kjk−1 T T Given these models, the Bayesian approach Sk HkPkjk−1Hk + MkRkLk T −1 aims to construct the posterior state distribution Kk Pkjk−1Hk Sk function p(xkjz1:k) given all the current measure- x^kjk x^kjk−1 + Kk(zk − h(x^kjk−1)) ments up to k. In the next subsections, brief re- Pkjk (I − KkHk)Pkjk−1 views of two famous techniques widely used in the attempt to construct such distribution are pre- end for sented. They are both non-linear extensions of the well known Kalman Filter, which provides the optimal estimator in the case in which the equa- 2.2 Unscented Kalman Filter tions (1) and (2) are linear and the noises and the initial distribution are Gaussian and mutually The EKF may perform poorly when the predic- independent. tion and observation functions are highly nonlin- ear. The Unscented Kalman Filter (UKF) uses a deterministic sampling technique, known as the 2.1 Extended Kalman Filter unscented transform (UT). This method better The Extended Kalman Filter (EKF) extends the approximates the posterior's true mean and co- original Kalman Filter by linearizing the models variance (Julier and Uhlmann, 2004). Therefore, given by equations (1) and (2) around the current the UKF often provides better estimate than the estimate. The extended Kalman Filter, despite EKF with similar computational cost. Addition- the non-linearities, still assumes that the state ally, the UKF does not require Jacobians com- probability function is Gaussian, even though that putations, which may be a hard task for very is not true in general for non-linear functions. The complex models. The UT carefully picks samples 1521 XIII Simp´osio Brasileiro de Automa¸c˜ao Inteligente Porto Alegre – RS, 1o – 4 de Outubro de 2017 (called sigma points) around the mean and prop- Algorithm 3 Function DrawSigmaPoints. agate them through the nonlinear function, from function DrawSigmaPoints(xa, Pa) which the mean and covariance of the estimate χ(0) = xa (0) λ are computed. Algorithm 2 shows a pseudocode wm = for the UKF, where the sigma points are selected n+λ w(0) = λ + 1 − α2 + β using the function DrawSigmaPoints, presented in c n+λ for i = 1; : : : ; n do Algorithm 3. χ(i) = xa + p(n + λ) Pa In the function DrawSigmaPoints, α and β :;i (i) (i) 1 are constants, where α determines the spread of wm = wc = 2(n+λ) the sigma points around the mean and is usually end for set to a small value (we use α = 10−3) and β = for i = n + 1;:::; 2n do 2 is the optimal value for gaussian distributions.
Recommended publications
  • A Neural Implementation of the Kalman Filter
    A Neural Implementation of the Kalman Filter Robert C. Wilson Leif H. Finkel Department of Psychology Department of Bioengineering Princeton University University of Pennsylvania Princeton, NJ 08540 Philadelphia, PA 19103 [email protected] Abstract Recent experimental evidence suggests that the brain is capable of approximating Bayesian inference in the face of noisy input stimuli. Despite this progress, the neural underpinnings of this computation are still poorly understood. In this pa- per we focus on the Bayesian filtering of stochastic time series and introduce a novel neural network, derived from a line attractor architecture, whose dynamics map directly onto those of the Kalman filter in the limit of small prediction error. When the prediction error is large we show that the network responds robustly to changepoints in a way that is qualitatively compatible with the optimal Bayesian model. The model suggests ways in which probability distributions are encoded in the brain and makes a number of testable experimental predictions. 1 Introduction There is a growing body of experimental evidence consistent with the idea that animals are some- how able to represent, manipulate and, ultimately, make decisions based on, probability distribu- tions. While still unproven, this idea has obvious appeal to theorists as a principled way in which to understand neural computation. A key question is how such Bayesian computations could be per- formed by neural networks. Several authors have proposed models addressing aspects of this issue [15, 10, 9, 19, 2, 3, 16, 4, 11, 18, 17, 7, 6, 8], but as yet, there is no conclusive experimental evidence in favour of any one and the question remains open.
    [Show full text]
  • Kalman and Particle Filtering
    Abstract: The Kalman and Particle filters are algorithms that recursively update an estimate of the state and find the innovations driving a stochastic process given a sequence of observations. The Kalman filter accomplishes this goal by linear projections, while the Particle filter does so by a sequential Monte Carlo method. With the state estimates, we can forecast and smooth the stochastic process. With the innovations, we can estimate the parameters of the model. The article discusses how to set a dynamic model in a state-space form, derives the Kalman and Particle filters, and explains how to use them for estimation. Kalman and Particle Filtering The Kalman and Particle filters are algorithms that recursively update an estimate of the state and find the innovations driving a stochastic process given a sequence of observations. The Kalman filter accomplishes this goal by linear projections, while the Particle filter does so by a sequential Monte Carlo method. Since both filters start with a state-space representation of the stochastic processes of interest, section 1 presents the state-space form of a dynamic model. Then, section 2 intro- duces the Kalman filter and section 3 develops the Particle filter. For extended expositions of this material, see Doucet, de Freitas, and Gordon (2001), Durbin and Koopman (2001), and Ljungqvist and Sargent (2004). 1. The state-space representation of a dynamic model A large class of dynamic models can be represented by a state-space form: Xt+1 = ϕ (Xt,Wt+1; γ) (1) Yt = g (Xt,Vt; γ) . (2) This representation handles a stochastic process by finding three objects: a vector that l describes the position of the system (a state, Xt X R ) and two functions, one mapping ∈ ⊂ 1 the state today into the state tomorrow (the transition equation, (1)) and one mapping the state into observables, Yt (the measurement equation, (2)).
    [Show full text]
  • Lecture 8 the Kalman Filter
    EE363 Winter 2008-09 Lecture 8 The Kalman filter • Linear system driven by stochastic process • Statistical steady-state • Linear Gauss-Markov model • Kalman filter • Steady-state Kalman filter 8–1 Linear system driven by stochastic process we consider linear dynamical system xt+1 = Axt + But, with x0 and u0, u1,... random variables we’ll use notation T x¯t = E xt, Σx(t)= E(xt − x¯t)(xt − x¯t) and similarly for u¯t, Σu(t) taking expectation of xt+1 = Axt + But we have x¯t+1 = Ax¯t + Bu¯t i.e., the means propagate by the same linear dynamical system The Kalman filter 8–2 now let’s consider the covariance xt+1 − x¯t+1 = A(xt − x¯t)+ B(ut − u¯t) and so T Σx(t +1) = E (A(xt − x¯t)+ B(ut − u¯t))(A(xt − x¯t)+ B(ut − u¯t)) T T T T = AΣx(t)A + BΣu(t)B + AΣxu(t)B + BΣux(t)A where T T Σxu(t) = Σux(t) = E(xt − x¯t)(ut − u¯t) thus, the covariance Σx(t) satisfies another, Lyapunov-like linear dynamical system, driven by Σxu and Σu The Kalman filter 8–3 consider special case Σxu(t)=0, i.e., x and u are uncorrelated, so we have Lyapunov iteration T T Σx(t +1) = AΣx(t)A + BΣu(t)B , which is stable if and only if A is stable if A is stable and Σu(t) is constant, Σx(t) converges to Σx, called the steady-state covariance, which satisfies Lyapunov equation T T Σx = AΣxA + BΣuB thus, we can calculate the steady-state covariance of x exactly, by solving a Lyapunov equation (useful for starting simulations in statistical steady-state) The Kalman filter 8–4 Example we consider xt+1 = Axt + wt, with 0.6 −0.8 A = , 0.7 0.6 where wt are IID N (0, I) eigenvalues of A are
    [Show full text]
  • Kalman-Filter Control Schemes for Fringe Tracking
    A&A 541, A81 (2012) Astronomy DOI: 10.1051/0004-6361/201218932 & c ESO 2012 Astrophysics Kalman-filter control schemes for fringe tracking Development and application to VLTI/GRAVITY J. Menu1,2,3,, G. Perrin1,3, E. Choquet1,3, and S. Lacour1,3 1 LESIA, Observatoire de Paris, CNRS, UPMC, Université Paris Diderot, Paris Sciences et Lettres, 5 place Jules Janssen, 92195 Meudon, France 2 Instituut voor Sterrenkunde, KU Leuven, Celestijnenlaan 200D, 3001 Leuven, Belgium e-mail: [email protected] 3 Groupement d’Intérêt Scientifique PHASE (Partenariat Haute résolution Angulaire Sol Espace) between ONERA, Observatoire de Paris, CNRS and Université Paris Diderot, France Received 31 January 2012 / Accepted 28 February 2012 ABSTRACT Context. The implementation of fringe tracking for optical interferometers is inevitable when optimal exploitation of the instrumental capacities is desired. Fringe tracking allows continuous fringe observation, considerably increasing the sensitivity of the interfero- metric system. In addition to the correction of atmospheric path-length differences, a decent control algorithm should correct for disturbances introduced by instrumental vibrations, and deal with other errors propagating in the optical trains. Aims. In an effort to improve upon existing fringe-tracking control, especially with respect to vibrations, we attempt to construct con- trol schemes based on Kalman filters. Kalman filtering is an optimal data processing algorithm for tracking and correcting a system on which observations are performed. As a direct application, control schemes are designed for GRAVITY, a future four-telescope near-infrared beam combiner for the Very Large Telescope Interferometer (VLTI). Methods. We base our study on recent work in adaptive-optics control.
    [Show full text]
  • The Unscented Kalman Filter for Nonlinear Estimation
    The Unscented Kalman Filter for Nonlinear Estimation Eric A. Wan and Rudolph van der Merwe Oregon Graduate Institute of Science & Technology 20000 NW Walker Rd, Beaverton, Oregon 97006 [email protected], [email protected] Abstract 1. Introduction The Extended Kalman Filter (EKF) has become a standard The EKF has been applied extensively to the field of non- technique used in a number of nonlinear estimation and ma- linear estimation. General application areas may be divided chine learning applications. These include estimating the into state-estimation and machine learning. We further di- state of a nonlinear dynamic system, estimating parame- vide machine learning into parameter estimation and dual ters for nonlinear system identification (e.g., learning the estimation. The framework for these areas are briefly re- weights of a neural network), and dual estimation (e.g., the viewed next. Expectation Maximization (EM) algorithm) where both states and parameters are estimated simultaneously. State-estimation This paper points out the flaws in using the EKF, and The basic framework for the EKF involves estimation of the introduces an improvement, the Unscented Kalman Filter state of a discrete-time nonlinear dynamic system, (UKF), proposed by Julier and Uhlman [5]. A central and (1) vital operation performed in the Kalman Filter is the prop- (2) agation of a Gaussian random variable (GRV) through the system dynamics. In the EKF, the state distribution is ap- where represent the unobserved state of the system and proximated by a GRV, which is then propagated analyti- is the only observed signal. The process noise drives cally through the first-order linearization of the nonlinear the dynamic system, and the observation noise is given by system.
    [Show full text]
  • 1 the Kalman Filter
    Macroeconometrics, Spring, 2019 Bent E. Sørensen August 20, 2019 1 The Kalman Filter We assume that we have a model that concerns a series of vectors αt, which are called \state vectors". These variables are supposed to describe the current state of the system in question. These state variables will typically not be observed and the other main ingredient is therefore the observed variables yt. The first step is to write the model in state space form which is in the form of a linear system which consists of 2 sets of linear equations. The first set of equations describes the evolution of the system and is called the \Transition Equation": αt = Kαt−1 + Rηt ; where K and R are matrices of constants and η is N(0;Q) and serially uncorrelated. (This setup allows for a constant also.) The second set of equations describes the relation between the state of the system and the observations and is called the \Measurement Equation": yt = Zαt + ξt ; where ξt is N(0;H), serially uncorrelated, and E(ξtηt−j) = 0 for all t and j. It turns out that a lot of models can be put in the state space form with a little imagination. The main restriction is of course on the linearity of the model while you may not care about the normality condition as you will still be doing least squares. The state-space model as it is defined here is not the most general possible|it is in principle easy to allow for non-stationary coefficient matrices, see for example Harvey(1989).
    [Show full text]
  • BDS/GPS Multi-System Positioning Based on Nonlinear Filter Algorithm
    Global Journal of Computer Science and Technology: G Interdisciplinary Volume 16 Issue 1 Version 1.0 Year 2016 Type: Double Blind Peer Reviewed International Research Journal Publisher: Global Journals Inc. (USA) Online ISSN: 0975-4172 & Print ISSN: 0975-4350 BDS/GPS Multi-System Positioning based on Nonlinear Filter Algorithm By JaeHyok Kong, Xuchu Mao & Shaoyuan Li Shanghai Jiao Tong University Abstract- The Global Navigation Satellite System can provide all-day three-dimensional position and speed information. Currently, only using the single navigation system cannot satisfy the requirements of the system's reliability and integrity. In order to improve the reliability and stability of the satellite navigation system, the positioning method by BDS and GPS navigation system is presented, the measurement model and the state model are described. Furthermore, Unscented Kalman Filter (UKF) is employed in GPS and BDS conditions, and analysis of single system/multi-systems’ positioning has been carried out respectively. The experimental results are compared with the estimation results, which are obtained by the iterative least square method and the extended Kalman filtering (EFK) method. It shows that the proposed method performed high-precise positioning. Especially when the number of satellites is not adequate enough, the proposed method can combine BDS and GPS systems to carry out a higher positioning precision. Keywords: global navigation satellite system (GNSS), positioning algorithm, unscented kalman filter (UKF), beidou navigation system (BDS). GJCST-G Classification : G.1.5, G.1.6, G.2.1 BDSGPSMultiSystemPositioningbasedonNonlinearFilterAlgorithm Strictly as per the compliance and regulations of: © 2016. JaeHyok Kong, Xuchu Mao & Shaoyuan Li. This is a research/review paper, distributed under the terms of the Creative Commons Attribution-Noncommercial 3.0 Unported License http://creativecommons.org/ licenses/by-nc/3.0/), permitting all non- commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.
    [Show full text]
  • E160 – Lecture 11 Autonomous Robot Navigation
    E160 – Lecture 11 Autonomous Robot Navigation Instructor: Chris Clark Semester: Spring 2016 1 Figures courtesy of Siegwart & Nourbakhsh A “cool” robot? https://www.youtube.com/watch?v=R8NXWkGzm1E 2 A “mobile” robot? http://www.theguardian.com/lifeandstyle/video/2015/feb/19/ 3 wearable-tomato-2015-tokyo-marathon-video Control Structures Planning Based Control Prior Knowledge Operator Commands Localization Cognition Perception Motion Control 4 ! Kalman Filter Localization § Introduction to Kalman Filters 1. KF Representations 2. Two Measurement Sensor Fusion 3. Single Variable Kalman Filtering 4. Multi-Variable KF Representations § Kalman Filter Localization 5 KF Representations § What do Kalman Filters use to represent the states being estimated? Gaussian Distributions! 6 KF Representations § Single variable Gaussian Distribution § Symmetrical § Uni-modal § Characterized by § Mean µ § Variance σ2 § Properties § Propagation of errors § Product of Gaussians 7 KF Representations § Single Var. Gaussian Characterization § Mean § Expected value of a random variable with a continuous Probability Density Function p(x) µ = E[X] = x p(x) dx § For a discrete set of K samples K µ = Σ xk /K k=1 8 KF Representations § Single Var. Gaussian Characterization § Variance § Expected value of the difference from the mean squared σ2 =E[(X-µ)2] = (x – µ)2p(x) dx § For a discrete set of K samples K 2 2 σ = Σ (xk – µ ) /K k=1 9 KF Representations § Single variable Gaussian Properties § Propagation of Errors 10 KF Representations § Single variable Gaussian Properties § Product of Gaussians 11 KF Representations § Single variable Gaussian Properties… § We stay in the “Gaussian world” as long as we start with Gaussians and perform only linear transformations.
    [Show full text]
  • Introduction to the Kalman Filter and Tuning Its Statistics for Near Optimal Estimates and Cramer Rao Bound
    Introduction to the Kalman Filter and Tuning its Statistics for Near Optimal Estimates and Cramer Rao Bound by Shyam Mohan M, Naren Naik, R.M.O. Gemson, M.R. Ananthasayanam Technical Report : TR/EE2015/401 arXiv:1503.04313v1 [stat.ME] 14 Mar 2015 DEPARTMENT OF ELECTRICAL ENGINEERING INDIAN INSTITUTE OF TECHNOLOGY KANPUR FEBRUARY 2015 Introduction to the Kalman Filter and Tuning its Statistics for Near Optimal Estimates and Cramer Rao Bound by Shyam Mohan M1, Naren Naik2, R.M.O. Gemson3, M.R. Ananthasayanam4 1Formerly Post Graduate Student, IIT, Kanpur, India 2Professor, Department of Electrical Engineering, IIT, Kanpur, India 3Formerly Additional General Manager, HAL, Bangalore, India 4Formerly Professor, Department of Aerospace Engineering, IISc, Banglore Technical Report : TR/EE2015/401 DEPARTMENT OF ELECTRICAL ENGINEERING INDIAN INSTITUTE OF TECHNOLOGY KANPUR FEBRUARY 2015 ABSTRACT This report provides a brief historical evolution of the concepts in the Kalman filtering theory since ancient times to the present. A brief description of the filter equations its aesthetics, beauty, truth, fascinating perspectives and competence are described. For a Kalman filter design to provide optimal estimates tuning of its statistics namely initial state and covariance, unknown parameters, and state and measurement noise covariances is important. The earlier tuning approaches are reviewed. The present approach is a reference recursive recipe based on multiple filter passes through the data without any optimization to reach a ‘statistical equilibrium’ solution. It utilizes the a priori, a pos- teriori, and smoothed states, their corresponding predicted measurements and the actual measurements help to balance the measurement equation and similarly the state equation to help form a generalized likelihood cost function.
    [Show full text]
  • MATH4406 (Control Theory) Part 10: Kalman Filtering and LQG 1 About
    MATH4406 (Control Theory) Part 10: Kalman Filtering and LQG Prepared by Yoni Nazarathy, Last Updated: October 19, 2012 1 About We have spent plenty of time in the course dealing with systems of the form: x_(t) = Ax(t) + Bu(t) x(n + 1) = Ax(n) + Bu(n) and : (1) y(t) = Cx(t) + Du(t) y(n) = Cx(n) + Du(n) with A 2 Rn×n, B 2 Rn×m, C 2 Rp×n and D 2 Rp×m. The focus was mostly on the continuous time version u(t); x(t); y(t). In unit 4 we saw how to design a state feedback controller and an observer and in later units we dealt with optimal control of such systems. We now augment our system models by adding noise components. To the first equation we shall add disturbance noise (ξx) and to the second equation we shall add measurement noise (ξy). This yields: x_(t) = Ax(t) + Bu(t) + ξ (t) x(n + 1) = Ax(n) + Bu(n) + ξ (n) x or x : y(t) = Cx(t) + Du(t) + ξy(t) y(n) = Cx(n) + Du(n) + ξy(n) One way of modeling the noise is by assuming that ξ(·) is from some function class and assuming that in controlling the system we have no knowledge of what specific ξ(·) from that class is used. This is the method of robust control. Alternatively, we can think of ξ(·) as a random process(es) by associating a probability space with the model. We shall focus on the latter approach.
    [Show full text]
  • GNSS/INS Integration Methods
    UNIVERSITA’ DEGLI STUDI DI NAPOLI “PARTHENOPE” Dipartimento di Scienze Applicate Dottorato di ricerca in Scienze Geodetiche e Topografiche XXIII Ciclo GNSS/INS Integration Methods Antonio Angrisano Supervisors: Prof. Mark Petovello, Prof. Mario Vultaggio Coordinatore: Prof. Lorenzo Turturici 2010 1 Abstract In critical locations such as urban or mountainous areas satellite navigation is difficult, above all due to the signal blocking problem; for this reason satellite systems are often integrated with inertial sensors, owing to their complementary features. A common configuration includes a GPS receiver and a high-precision inertial sensor, able to provide navigation information during GPS gaps. Nowadays the low cost inertial sensors with small size and weight and poor accuracy are developing and their use as part of integrated navigation systems in difficult environments is under investigation. On the other hand the recent enhancement of GLONASS satellite system suggests the combined use with GPS in order to increase the satellite availability as well as position accuracy; this can be especially useful in places with lack of GPS signals. This study is to assess the effectiveness of the integration of GPS/GLONASS with low cost inertial sensors in pedestrian and vehicular urban navigation and to investigate methods to improve its performance. The Extended Kalman filter is used to merge the satellite and inertial information and the loosely and tightly coupled integration strategies are adopted; their performances comparison in difficult areas is one of the main objectives of this work. Generally the tight coupling is more used in urban or natural canyons because it can provide an integrated navigation solution also with less than four satellites (minimum number of satellites necessary for a GPS only positioning); the inclusion of GLONASS satellites in this context may change significantly the role of loosely coupling in urban navigation.
    [Show full text]
  • GLONASS Inter-Frequency Phase Bias Rate Estimation by Single-Epoch Or Kalman Filter Algorithm
    GPS Solut DOI 10.1007/s10291-017-0660-3 ORIGINAL ARTICLE GLONASS inter-frequency phase bias rate estimation by single- epoch or Kalman filter algorithm 1,2,3 1 4 1 Yibin Yao • Mingxian Hu • Xiayan Xu • Yadong He Received: 23 April 2017 / Accepted: 18 August 2017 Ó Springer-Verlag GmbH Germany 2017 Abstract GLONASS double-differenced (DD) ambiguity the single-epoch IFB rate estimation algorithm can meet resolution is hindered by the inter-frequency bias (IFB) in the requirements for real-time kinematic positioning with GLONASS observation. We propose a new algorithm for only 8% extra computational time, and that the Kalman IFB rate estimation to solve this problem. Although the filter-based IFB rate estimation algorithm is a satisfactory wavelength of the widelane observation is several times option for high-accuracy GLONASS positioning. that of the L1 observation, their IFB errors are similar in units of meters. Based on this property, the new algorithm Keywords Multi-global navigation satellite system can restrict the IFB effect on widelane observation within (GNSS) Á Real-time kinematic (RTK) positioning Á 0.5 cycles, which means the GLONASS widelane DD GLONASS integer ambiguity resolution Á Inter-frequency ambiguity can be accurately fixed. With the widelane bias (IFB) integer ambiguity and phase observation, the IFB rate can be estimated using single-epoch measurements, called the single-epoch IFB rate estimation algorithm, or using the Introduction Kalman filter to process all data, called the Kalman filter- based IFB rate estimation algorithm. Due to insufficient GPS real-time kinematic (RTK) has become a reliable and accuracy of the IFB rate estimated from widelane obser- widespread algorithm for accurate positioning.
    [Show full text]