@inproceedings{5d475ef057ef450fb178bea496c2e36f,
title = "Development of a lateral-directional envelop protection flight control system",
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.",
keywords = "Aircraft, Command compensation, Envelop limit, Envelop protection, Flight control system, Lateraldirectional control, Simulation",
author = "Liu Fan and Wang Lixin",
year = "2012",
language = "英语",
isbn = "9789491216008",
series = "Proceedings of the 2012 International Conference on Computer Application and System Modeling, ICCASM 2012",
pages = "1177--1180",
booktitle = "Proceedings of the 2012 International Conference on Computer Application and System Modeling, ICCASM 2012",
note = "2012 2nd International Conference on Computer Application and System Modeling, ICCASM 2012 ; Conference date: 27-07-2012 Through 29-07-2012",
}