@inproceedings{f397f18f74ff42bc9cc5fc718c0183a4,
title = "Research on control allocation for aircrafts with multiple control effectors",
abstract = "This paper discusses the control allocation principle and solution for aircrafts with multiple control effectors from the angle of flight performance. ADMIRE developed by FOI is taken as example, and the control selector for ADMIRE is redesigned based on the control allocation principle and solution developed in this paper. The trimmed lift to drag ratio (L/D) and Combat Cycle Time (CCT) of ADMIRE with its original control selector and with the selector redesigned in this paper are compared, the results indicate that the principle and solution built in this paper are reasonable.",
keywords = "Control allocation, Flight performance, Multiple control effectors",
author = "Liu Yan and Gao Zheng-hong",
year = "2008",
language = "英语",
isbn = "9781605607153",
series = "ICAS Secretariat - 26th Congress of International Council of the Aeronautical Sciences 2008, ICAS 2008",
pages = "1619--1624",
booktitle = "ICAS Secretariat - 26th Congress of International Council of the Aeronautical Sciences 2008, ICAS 2008",
note = "26th Congress of International Council of the Aeronautical Sciences 2008, ICAS 2008 ; Conference date: 14-09-2008 Through 19-09-2008",
}