发明名称 Guided projectile flight control fin system
摘要 A guidance system for small spinning projectiles which is mechanically simple, has low power requirements, uses relatively unsophisticated electronics, and is capable of withstanding large gas pressures and accelerations. The system uses a one-piece fin assembly which is de-spun so that its guidance fins maintain a constant attitude with respect to the ground. The guidance fins and their hub can be nutated simultaneously and independently in two orthogonal planes by pivoting and translating a single control rod. The hub cooperates with the projectile body to reduce its base drag and thereby extend its range.
申请公布号 US4565340(A) 申请公布日期 1986.01.21
申请号 US19840641137 申请日期 1984.08.15
申请人 FORD AEROSPACE & COMMUNICATIONS CORPORATION 发明人 BAINS, WILLIAM R.
分类号 F42B10/64 主分类号 F42B10/64
代理机构 代理人
主权项
地址