Simultaneous lateral thrust and aerodynamic control of an agile missile

Hui Zou, Wanchun Chen, Peng Wang, Xingliang Yin

Research output: Contribution to journalArticlepeer-review

2 Scopus citations

Abstract

The blended control of a tail-controlled agile missile with attitude control motors is discussed. A controller, including aerodynamic control surface and pulse type lateral jets, was developed. It was divided into two parts: the control law and the blend logic. The control law can be designed easily as before, and the blend logic commands the two actuators. Simulations had been carried out to show the performance. Effect of the distance between motors and the center of gravity of the interceptor had also been discussed.

Original languageEnglish
Pages (from-to)192-196
Number of pages5
JournalBeijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
Volume30
Issue number3
StatePublished - Mar 2004
Externally publishedYes

Keywords

  • Attitude control
  • Blended control
  • Guided missile control
  • Impulse control
  • Rocket thrust

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