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유도탄의 유도명령 추종을 위한 혼합제어기 설계: 공력 및 추력벡터제어

Title
유도탄의 유도명령 추종을 위한 혼합제어기 설계: 공력 및 추력벡터제어
Other Titles
Mixed Control of Agile Missile with Aerodynamic Fin and Thrust Vectoring Control
Author
송택렬
Keywords
dynamic inversion; extended-mean assignment; control allocation; mixed control; linear time-varying system; autopilot; agile missile
Issue Date
2004-07
Publisher
제어·자동화·시스템공학회
Citation
제어·자동화·시스템공학논문지, v. 10, No. 7, Page. 658-568
Abstract
This paper is concerned with a control allocation strategy using the dynamic inversion and the pseudo inverse control which generates the nominal control input trajectories. In addition, an autopilot design method is proposed by using time-varying control technique which is missile with aerodynamic fin and thrust 7 time-varying version of the pole placement of linear time-invariant system for an agile vectoring control. The control allocation proposed in this paper is capable of extracting the maximum performance by combining each control effector, aerodynamic fm and thrust vectoring control. The adopted time-varying control technique for the autopilot design enhances the robustness of the tracking performance for a reference command. The main results are validated through the nonlinear simulations with aerodynamic data.
URI
http://www.dbpia.co.kr/journal/articleDetail?nodeId=NODE01968487&language=ko_KRhttps://repository.hanyang.ac.kr/handle/20.500.11754/151373
ISSN
1976-5622; 2233-4335
Appears in Collections:
COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > ELECTRICAL ENGINEERING(전자공학부) > Articles
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