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MISSILES AND GUIDANCE TECHNOLOGY

The Study on Robust Design of Tailless UAV 's Full Envelope Flight Control

  • CHENG Xuemei
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  • Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2010-04-18

  Online published: 2025-05-30

Abstract

The full envelope robust control of high-altitude-high-speed tailless UAV is a difficult point because of its wide envelope and non-conventional layout. In this paper, the robust control design was divided into two steps: firstly, solve the robust stability of tailless layout airplane; secondly, account for robust track of full envelope flight mode in mission section, and then the suitable full envelope robust control structure and method were given. The simulation shows that the control structure is robust from low altitude and low speed to high altitude and high speed.

Cite this article

CHENG Xuemei . The Study on Robust Design of Tailless UAV 's Full Envelope Flight Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(1) : 23 -25,32 . DOI: 10.15892/j.cnki.djzdxb.2011.01.025

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