The Extended H∞ Particle Filter for Attitude Estimation Applied to Remote Sensing Satellite CBERS-4

Author:

Silva William Reis1ORCID,Garcia Roberta Veloso2ORCID,Pardal Paula C. P. M.3ORCID,Kuga Hélio Koiti4ORCID,Zanardi Maria Cecília F. P. S.5ORCID,Baroni Leandro6ORCID

Affiliation:

1. Gama Campus (FGA), University of Brasilia (UnB), Área Especial de Indústria, Projeção A, Setor Leste (Gama), Brasília 72444-240, DF, Brazil

2. Lorena School of Engineering (EEL), University of São Paulo (USP), Estrada Municipal do Campinho, S/N. Ponte Nova, Lorena 12602-810, SP, Brazil

3. Collaborative Laboratory (CoLAB), Center of Engineering and Product Development (CEiiA), PACT, Rua Luís Adelino Fonseca, 1, 7005-841 Évora, Portugal

4. Space Mechanics and Control Division (DMC), National Institute for Space Research (INPE), Av. dos Astronautas, 1758, Jardim da Granja, São José dos Campos 12227-010, SP, Brazil

5. Campus Guaratinguetá (FEG), São Paulo State University (UNESP), Av. Dr. Ariberto Pereira da Cunha, 333, Pedregulho, Guaratinguetá 12516-410, SP, Brazil

6. Engineering, Modeling and Applied Social Sciences Center (CECS), Federal University of ABC (UFABC), Av. dos Estados, 5001, Bangú, Santo André 09210-580, SP, Brazil

Abstract

An extension of the linear H∞ filter, presented here as the extended H∞ particle filter (EH∞PF), is used in this work for attitude estimation, which presents a process and measurement model with nonlinear functions. The simulations implemented use orbit and attitude data from CBERS-4 (China–Brazil Earth Resources Satellite-4), making use of the robustness characteristics of the H∞ filter. The CBERS-4 is the fifth satellite of an advantageous international scientific interaction between Brazil and China for the development of remote sensing satellites used for strategic application in monitoring water resources and controlling deforestation in the Legal Amazon. In the extended H∞ particle filter (EH∞PF) the nature of the system, composed of dynamics and noises, seeks to degrade the state estimate. The EH∞PF deals with this by aiming for robustness, using a performance parameter in its cost function, in addition to presenting an advantageous feature of using a reduced number of particles for state estimation. The justification for the application of this method is because the non-Gaussian uncertainties that appear in the attitude sensors impair the estimation process and the EH∞PF minimizes in signal estimation the worst effects of disturbance signals without a priori knowledge of them, as shown in the results, in addition to presenting good precision within the prescribed requirements, with 100 particles representing a processing time 2.09 times less than the PF with 500 particles.

Funder

National Council for Scientific and Technological Development

Publisher

MDPI AG

Subject

General Earth and Planetary Sciences

Reference33 articles.

1. Spacecraft Attitude Estimation using Unscented Kalman Filters, Regularized Particle Filter and Extended H∞ Filter;Silva;Adv. Astronaut. Sci.,2017

2. Advances in Microprocessor Cache Architectures Over the Last 25 Years;Iyer;IEEE Micro,2021

3. Simon, D. (2006). Optimal State Estimation, Kalman, H∞, and Nonlinear Approaches, Wiley.

4. Singular value decomposition based robust cubature Kalman filtering for an integrated GPS/SINS navigation system;Zhang;J. Navig.,2014

5. Banavar, R. (1992). A Game Theoretic Approach to Linear Dynamics Estimation. [Ph.D. Thesis, University of Texas at Austin].

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