Separation section is the most complex and dramatic stage in disturbing the cruise missile during the entire flight trajectory. The characteristic of low-altitude, low-speed, non-aileron flight separation of the missile propelled by rocket was analyzed in this paper. Classic engineering methods and neural network dynamic inversion methods was used to design control system, and two different control methods were compared.
One Kind of Flight Control System Design for Separation Section in Cruise Missile
Advanced Materials Research ; 490-495 ; 885-889
2012-03-15
5 pages
Article (Journal)
Electronic Resource
English
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