Development of a Lateral-directional Envelop Protection Flight Control System

DOI

10.2991/iccasm.2012.300How to use a DOI?

Keywords

Aircraft, Envelop protection, Envelop limit, Command compensation, Flight control system, Lateraldirectional control, Simulation

Abstract

For the factor of aircraft flying safety, some critical flight parameters must be limited within the envelop borders. However, excellent flight performance requires that the aircraft can flight to some envelop borders easily and fast nearly. The purpose of envelop protection is to solve this dilemma. Based on the basic lateral-directional flight control law, an envelop protection method using control command compensation is developed. Numerical simulation results show that this method can effectively solves the flying safety problem without sacrificing flight performance.

Copyright

© 2012, 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  - Fan Liu
AU  - Lixin Wang
PY  - 2012/08
DA  - 2012/08
TI  - Development of a Lateral-directional Envelop Protection Flight Control System
BT  - Proceedings of the 2012 International Conference on Computer Application and System Modeling (ICCASM 2012)
PB  - Atlantis Press
SP  - 1177
EP  - 1180
SN  - 1951-6851
UR  - https://doi.org/10.2991/iccasm.2012.300
DO  - 10.2991/iccasm.2012.300
ID  - Liu2012/08
ER  -