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Based On The Matrixx The Missile Attitude Control System Design

Posted on:2002-03-21Degree:MasterType:Thesis
Country:ChinaCandidate:H YaoFull Text:PDF
GTID:2192360065961454Subject:Aircraft design
Abstract/Summary:PDF Full Text Request
The paper disscuses about the ballistic missile attitude control system design problem.By analyzing the features of the control system model and the process of the controller design, develop simulation software used on design of the attitude control system based on MATRIXx,so as to reflect the property of classical design method -. improve the efficiency of controller design.The simulation software MATRIXx is used as developing platform which improves researcher's efficiency and enhances designed software's reliability and readability .The paper applies H design method to design of the missile attitude control system ,andcompares with the classical design method in order to acquire the controller with better performance.The content configuration of the paper is: Chapter 1 describes the features of the missile attitude control system design; Chapter 2 bring forward the dynamics model of the missile attitude control system; Chapter 3 describes the characteristices of the missile attitude control system design, emphases on the analyse of stability and the flexibility stability; Chapter 4 illustrates the simulation software design of the missile attitude control system. Chapter 5 applies Hx design method to the missile attitude control system design; Chapter 6 describes the design of simulation software on the three-channel for system.
Keywords/Search Tags:Missile Attitude Control, Software design, Ha, MATRIXx
PDF Full Text Request
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