The Study on Robust Design of Tailless UAV 's Full Envelope Flight Control
Received date: 2010-04-18
Online published: 2025-05-30
程雪梅 . 高空高速无尾布局无人机全包线鲁棒控制设计研究[J]. 弹箭与制导学报, 2011 , 31(1) : 23 -25,32 . DOI: 10.15892/j.cnki.djzdxb.2011.01.025
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.
Key words: high-altitude-high-speed; tailless UAV; full envelope; robust control
| [1] | Paul R. Garrard WL. Dynamic and control of tailless aircraft, AIAA-97-3776[R]. 1997. |
| [2] | Esteban S. Static and dynamic analysis of an unconventional plane: flying wing, AIAA-2001-4010[R]. 2001. |
| [3] | 郭锁凤. B-2飞行控制系统的设计技术[J]. 国际航空, 1994(8): 57-58. |
| [4] | 熊治国, 董新民. 程序调参飞行控制律的研究与展望[J]. 飞行力学, 2003, 21(4): 9-13. |
| [5] | Shamma J S, Athans M. Analysis of gain scheduled control for nonlinear plants[J]. IEEE Transaction on Automatic Control, 1990, 35(8): 898-907. |
| [6] | Kuang-Hsuan Tu, Shamma J S. Nonlinear gain scheduled control design using set-valued methods[C]// Proceeding of American Control Conference, 1998: 1195-1199. |
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