DocumentCode
1795313
Title
Disturbance observer based constrained multi-model predictive control for Mars entry trajectory tracking
Author
Wu Chao ; Li Shihua ; Yang Jun ; Guo Lei
Author_Institution
Sch. of Autom., Southeast Univ. & Key Lab. of Meas. & Control of Complex Syst. of Eng., Nanjing, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
2341
Lastpage
2346
Abstract
For future Mars entry missions, a composite entry tracking strategy is studied in this article. For precision entry, the nonlinear entry dynamics, complex uncertainties and multi-source disturbance are considered specially. The composite entry tracking strategy includes constrained multi-model predictive control (CMPC), to optimize tracking performance, as well as disturbance observer based control for active disturbance rejection. Monte Carlo simulations demonstrate the effectiveness of the proposed method under control saturation constraint, multi-source disturbances and uncertainties of initial states and aerodynamic parameters.
Keywords
Monte Carlo methods; active disturbance rejection control; aerodynamics; aerospace control; observers; predictive control; trajectory control; vehicle dynamics; Mars entry missions; Mars entry trajectory tracking; Monte Carlo simulations; active disturbance rejection; aerodynamic parameters; complex uncertainties; composite entry tracking strategy; constrained multimodel predictive control; control saturation constraint; disturbance observer based control; initial state uncertainties; multisource disturbance; nonlinear entry dynamics; precision entry; Aerodynamics; Mars; Mathematical model; Trajectory; Uncertainty; Vehicle dynamics; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007534
Filename
7007534
Link To Document