Lateral-directional Attitude Under-actuated Control Strategy of Hypersonic Vehicle

DOI

10.2991/icsma-16.2016.71How to use a DOI?

Keywords

Hypersonic vehicle, Under-actuated, Cascade control.

Abstract

Research on lateral-directional attitude under-actuated control of the hypersonic vehicle with only the aileron, a new lateral-directional control strategy based on the idea of cascade was proposed, that can realize the roll angle control and guarantee the stabilization of the sideslip angle. Using the linear lateral-directional dynamic equations, the under-actuated control mechanism was analyzed. The rudder could produce sideslip angle, and the roll angle could be controlled by sideslip angle. With the concept of cascade control, a controller of two levels was designed that was seriesÿconnection of the roll angle controller and sideslip angle controller. Results show that the design of the lateral-directional cascade control strategy can stabilize the system and the tacking performance of the roll angle satisfies the requirement.

Copyright

© 2016, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yike Niu
AU  - Chunzhen Sun
AU  - Yimin Huang
AU  - Xin Wang
PY  - 2016/12
DA  - 2016/12
TI  - Lateral-directional Attitude Under-actuated Control Strategy of Hypersonic Vehicle
BT  - Proceedings of the 2016 4th International Conference on Sensors, Mechatronics and Automation (ICSMA 2016)
PB  - Atlantis Press
SP  - 399
EP  - 404
SN  - 1951-6851
UR  - https://doi.org/10.2991/icsma-16.2016.71
DO  - 10.2991/icsma-16.2016.71
ID  - Niu2016/12
ER  -