Full Text:   <814>

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CLC number: TP273; V448.2

On-line Access: 2017-05-24

Received: 2015-12-21

Revision Accepted: 2016-02-26

Crosschecked: 2017-04-16

Cited: 0

Clicked: 1759

Citations:  Bibtex RefMan EndNote GB/T7714

 ORCID:

Gong-jun Li

http://orcid.org/0000-0001-8503-2973

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Frontiers of Information Technology & Electronic Engineering  2017 Vol.18 No.5 P.599-614

10.1631/FITEE.1500464


Adaptive tracking control for air-breathing hypersonic vehicles with state constraints


Author(s):  Gong-jun Li

Affiliation(s):  Science and Technology on Space Intelligent Control Laboratory, Beijing Institute of Control Engineering, Beijing 100190, China

Corresponding email(s):   gongjun_bice@buaa.edu.cn

Key Words:  Hypersonic vehicle, Constraints, Output redefinition, Barrier Lyapunov function


Gong-jun Li. Adaptive tracking control for air-breathing hypersonic vehicles with state constraints[J]. Frontiers of Information Technology & Electronic Engineering, 2017, 18(5): 599-614.

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Abstract: 
We investigate the adaptive tracking problem for the longitudinal dynamics of state-constrained air-breathing hypersonic vehicles, where not only the velocity and the altitude, but also the angle of attack (AOA) is required to be tracked. A novel indirect AOA tracking strategy is proposed by viewing the pitch angle as a new output and devising an appropriate pitch angle reference trajectory. Then based on the redefined outputs (i.e., the velocity, the altitude, and the pitch angle), a modified backstepping design is proposed where the barrier Lyapunov function is used to solve the state-constrained control problem and the control gain of this class of systems is unknown. Stability analysis is given to show that the tracking objective is achieved, all the closed-loop signals are bounded, and all the states always satisfy the given constraints. Finally, numerical simulations verify the effectiveness of the proposed approach.

This paper investigates the adaptive tracking problem for the longitudinal dynamics of state-constrained air-breathing hypersonic vehicles. The angle of attack (AOA) is constrained by applying to the propose control scheme. This research topic is interesting.

状态受限吸气式高超声速飞行器自适应跟踪控制

概要:本文研究了纵向通道吸气式高超声速飞行器的状态受限自适应跟踪控制问题,其中,速度、高度和攻角均要求跟踪给定的参考曲线。通过选择俯仰角作为新的输出并设计合适的俯仰角参考曲线,提出了一种新颖的间接攻角跟踪策略。基于重新定义的输出(即:速度、高度和俯仰角),给出了一种基于修正的退步控制器设计方法,其中,障碍李雅普诺夫函数用来求解控制增益未知情况下的状态受限控制问题。稳定性分析表明本方法实现了跟踪控制的目标,同时所有的闭环信号有界,状态始终满足给定约束。数值仿真验证了本方法的有效性。

关键词:高超声速飞行器;约束;输出重定义;障碍李雅普诺夫函数

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

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