NDLI: Reentry vehicle modeling and sliding mode controller design

Content Provider	IEEE Xplore Digital Library
Author	Peng Wang Luhua Liu Jie Wu Wei Zheng
Copyright Year	2011
Description	Author affiliation: College of Aerospace and Materials Engineering, National University of Defense Technology, NUDT, Changsha, China (Peng Wang; Luhua Liu; Jie Wu; Wei Zheng)
Abstract	A Six Degrees of Freedom(Six-DoF) reentry vehicle model is being developed for control studies. This vehicle model is highly nonlinear, multivariable, unstable and coupling and includes uncertain parameters. The dynamic inverse method and sliding mode control are used in inner-loop and outer-loop for the reentry vehicle control respectively according to the dynamic equations. When dynamic inversion decoupling technology is applied to the vehicle model, the output dynamics for pitch angle, yaw angle and rolling angle can be derived by differentiating two times respectively. The relative degree equals to the rotational motion system order. Thus, rotational motion dynamic model can be Input/Output linearized completely and is decoupled. A multi-input/multi-output(MIMO) sliding mode controller is designed based on the linearized model. Saturation function is applied to reduce the chattering of the slide mode. Simulation studies are conducted for initial conditions of altitude of 60km and Mach 20 for the responses of the commands of angle of attack, sideslip angle and bank angle. The simulation studies demonstrate that the proposed controller is robust with respect to the interference and parametric uncertainties, and meets the performance requirements with acceptable control inputs.
Starting Page	227
Ending Page	231
File Size	1240400
Page Count	5
File Format	PDF
ISBN	9781424496174
e-ISBN	9781424496167
DOI	10.1109/RAST.2011.5966829
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-06-09
Publisher Place	Turkey
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	sliding mode control decoupling robustness reentry vehicle Aerodynamics dynamic inversion Robustness Mathematical model Vehicle dynamics Sliding mode control Equations Vehicles
Content Type	Text
Resource Type	Article

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