首页>
外国专利>
IN-FLIGHT ATTITUDE CONTROL AND DIRECT THRUST FLIGHT CONTROL SYSTEM OF A VEHICLE AND CRAFT COMPRISING SUCH A SYSTEM
IN-FLIGHT ATTITUDE CONTROL AND DIRECT THRUST FLIGHT CONTROL SYSTEM OF A VEHICLE AND CRAFT COMPRISING SUCH A SYSTEM
展开▼
机译:包括这种系统的车辆和飞机的飞行中姿态控制和直接推力飞行控制系统
展开▼
页面导航
摘要
著录项
相似文献
摘要
A system for in-flight attitude control and side-force steering includes a thruster body and a plurality of valves capable of generating side thrusts put into communication with the thruster body. The valves are arranged in two sets of valves spaced apart from each other towards the front and towards the rear of the thruster body in substantially symmetrical manner relative to the center of gravity of the vehicle situated on a longitudinal axis (A) of the vehicle. Each set comprises a first pair of valves generating thrust in opposite directions along axes that are not in alignment and are parallel to a first axis, and a second pair of valves generating thrust in opposite directions along axes that are not aligned and are parallel to a second axis. The first and second axes are distinct and perpendicular to the longitudinal axis of the vehicle.
展开▼