DocumentCode :
3550032
Title :
Flatness based real-time trajectory generation for acceleration control of agile STT missile with constraints
Author :
Li, Congying ; Tang, Daquan ; Shang, Anli ; Gu, Wenjin ; Wang, Ruiqi
Author_Institution :
Postgraduate Students Brigade, NAEI, Yantai, China
Volume :
3
fYear :
2004
fDate :
6-9 Dec. 2004
Firstpage :
1917
Abstract :
In order to deal with nonminimum phase problem in acceleration control of agile STT missiles, a new VSC control method was introduced, from which flat output was constructed. Real-time trajectory generation algorithm based on flatness was constructed to deal with unavoidable constraints in missile control system. Simulation was made for verification. Simulation results showed the effectiveness and correctness of the flatness based trajectory generation algorithm.
Keywords :
acceleration control; missile control; variable structure systems; STT missile; VSC control method; acceleration control; flatness based real-time trajectory generation; missile control system; nonminimum phase problem; unavoidable constraint; Acceleration; Accelerometers; Algorithm design and analysis; Automatic control; Automatic generation control; Control systems; Equations; Missiles; Nonlinear dynamical systems; Real time systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation, Robotics and Vision Conference, 2004. ICARCV 2004 8th
Print_ISBN :
0-7803-8653-1
Type :
conf
DOI :
10.1109/ICARCV.2004.1469453
Filename :
1469453
Link To Document :
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