Adaptive attitude controller of a reentry vehicles based on Back-stepping Dynamic inversion method

Mohseni, A.; Fani Saberi, F.; Mortazavi, M.

doi:10.22060/miscj.2017.12907.5048

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	Adaptive attitude controller of a reentry vehicles based on Back-stepping Dynamic inversion method
Article 10, Volume 50, Issue 1, Winter and Spring 2018, Page 95-106 PDF (704 K)
Document Type: Review Article
DOI: 10.22060/miscj.2017.12907.5048
Authors
A. Mohseni¹; F. Fani Saberi ²; M. Mortazavi¹
¹Department of Aerospace Engineering, Amirkabir University of Technology, 15875-4413, Tehran, Iran.
²Space Science and Technology Institute, Amirkabir University of Technology, 15875-4413, Tehran, Iran.
Abstract
This paper presents an attitude control algorithm for a Reusable Launch Vehicle (RLV) with a low lift/drag ratio (L/D < 0.5), in presence of external disturbances, model uncertainties, control output constraints and the thruster model. The main novelty of the proposed control strategy is a new combination of the attitude control methods including backstepping, dynamic inversion, and adaptive control methods which will be called Backstepping-Dynamic inversion-Adaptive (B.D.A) method. In the proposed method, a single control variable is considered as the bank angle while the angle of the attack and the side slip angle will be stabilized in their inherent value. The purpose of this control is the attitude control of the vehicle to track the commanded bank angle and keep the vehicle in the desired trajectory. Lyapunov stability analysis of the closed-loop system will be performed to guaranty the stability of the vehicle in the presence of constraints. Performance of the controller will be evaluated based on six Degrees of Freedom (6-DOF) model of the re-entry capsule. Also, the results of the proposed control algorithm will be compared with the Backstepping Dynamic inversion (B.D) control method.
Keywords
Attitude control; Backstepping-Dynamic inversion-Adaptive; Reusable Launch Vehicle (RLV); Controller output constraint; Thruster model
Main Subjects
Adaptive Control; Aeronautical systems; Classical Nonlinear System Control; Robust Control


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