发明名称 GUIDANCE CONTROL FOR SPINNING OR ROLLING PROJECTILE
摘要 A projectile, air vehicle or submersible craft with a spinning or rolling fuselage, rotating on its axis, has a collar which can be positioned relative to a longitudinal axis of the projectile using aerodynamic forces. Aerodynamic surfaces, such as lift-producing surfaces, for example tails or canards, are coupled to the collar, and rotate with the collar. An actuator system or mechanism controls orienting of the lift-producing surfaces, such as tilting of the lift producing surfaces, to direct the collar into a desired position relative to a longitudinal axis of the projectile, and to maintain the collar in that position. With such a control the projectile is able to be steered using bank-to-turn maneuvering. The actuator system may use any of a variety of mechanisms to move the lift-producing surfaces, thereby positioning the collar.
申请公布号 US2012175458(A1) 申请公布日期 2012.07.12
申请号 US201113005175 申请日期 2011.01.12
申请人 GESWENDER CHRIS E. 发明人 GESWENDER CHRIS E.
分类号 F42B15/01;F42B10/00;F42C14/00 主分类号 F42B15/01
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