System and method for attitude control of a flight vehicle...

F - Mech Eng,Light,Heat,Weapons – 42 – B

Patent

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F42B 10/66 (2006.01)

Patent

CA 2644597

A reliable and inexpensive attitude control system uses a plurality of pitch-over thrusters to perform rapid and precise attitude maneuvers for a flight vehicle. The pitch- over thrusters create rotational moments that directly pitch and yaw the flight vehicle. The use of very simple thrusters and control techniques provides for a reliable and cost effective solution. The ability to perform overlapping pitch and yaw maneuvers with single-shot fixed-impulse thrusters provides for high-speed maneuverability.

L'invention concerne un système de régulation d'attitude fiable et peu coûteux faisant appel à une pluralité de propulseurs de basculement en vue de la réalisation de manoeuvres d'attitude rapides et précises pour un véhicule volant. Les propulseurs de basculement créent des moments de rotation provoquant le tangage et le lacet du véhicule volant. L'utilisation de propulseurs et de techniques de commande très simples permet d'obtenir une solution fiable et peu coûteuse. La possibilité de réaliser simultanément des manoeuvres de tangage et de lacet au moyen de propulseurs à impulsion fixe à un coup permet d'obtenir une manoeuvrabilité à vitesse élevée.

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