Control Allocation–Based Command Tracking–Control System for Hypersonic Re-entry Vehicle Driven by Hybrid Effecters-Reference-Cited by-同舟云学术

Control Allocation–Based Command Tracking–Control System for Hypersonic Re-entry Vehicle Driven by Hybrid Effecters

Published:2018-07 Issue:4 Volume:31 Page:04018031
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Song Jianmei¹,Cai Gaohua²,Chen Xianxiang³

Affiliation:

1. Associate Professor and Ph.D. Tutor, Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, No. 5 South Zhongguancun St., Haidian District, Beijing 100081, P.R. China (corresponding author).

2. Engineer, System Scheme R&D Dept., Beijing Aerospace Automatic Control Institute, No. 50, Yongding St., Haidian District, Beijing 100854, P.R. China.

3. Engineer, Intelligent System Control R&D Dept., Beijing Institute of Computer Application, No. 10, Chedaogou St., Haidian District, Beijing 100089, P.R. China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000855

Reference19 articles.

1. Ahmad H. Young T. M. Toal D. and Omerdic E. (2007). “Control allocation with actuator dynamics for aircraft flight controls.” 7th AIAA Aviation Technology Integration and Operations Conf. AIAA Reston VA.

2. Flight control system design for hypersonic reentry vehicle based on LFT–LPV method

3. Robust LPV autopilot design for hypersonic reentry vehicle

4. Command Tracking Control System Design and Evaluation for Hypersonic Reentry Vehicles Driven by a Reaction Control System

5. Control system design for hypersonic reentry vehicle driven by aerosurfaces and reaction control system

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