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This paper presents an adaptive flight control system for a launch vehicle. The rocket has an in-line configuration with each stage on top to another and the payload placed atop the rocket. The driving is achieved through the reactive rocket engine gimbaled nozzle, by changing the orientation of the thrust force. Rocket rotation around roll axis is done through two reactive engines placed near the...
The paper deals with a mathematical model for airplanes' longitudinal movement during the approach-stage of the landing. One has described an aerodynamic decelerated approach and has established the correlation between airplane's flight commands and thrust level (engines' commands). Airplane's command law was issued (a common law, for rudder and throttle positions), according to the approach law,...
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