Dynamic Inverse Based Controller for a Hypersonic Flight Vehicle

DOI

10.2991/icismme-15.2015.71How to use a DOI?

Keywords

hypersonic vehicle; sliding mode control; Feedback linearization

Abstract

A dynamic inverse based controller is designed for the longitudinal dynamics of a generic hypersonic vehicle. This model is strong nonlinear, multivariable coupling and includes uncertain parameters based on its high speed, lager aerodynamic load and rapid changing flight area. After feedback linearization of original model to get dynamic inverse linear model, optimal control method is used to develop controller to follow height and velocity commands. Simulation studies demonstrate that this controller is capable to follow height and speed change commands rapidly and accurately with certain robustness.

Copyright

© 2015, 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  - Lindong Zhao
AU  - Shengjing Tang
PY  - 2015/07
DA  - 2015/07
TI  - Dynamic Inverse Based Controller for a Hypersonic Flight Vehicle
BT  - Proceedings of the First International Conference on Information Sciences, Machinery, Materials and Energy
PB  - Atlantis Press
SP  - 360
EP  - 363
SN  - 1951-6851
UR  - https://doi.org/10.2991/icismme-15.2015.71
DO  - 10.2991/icismme-15.2015.71
ID  - Zhao2015/07
ER  -