飞行器滚转尾翼设计

Design and Test of Rolling Tail for Flight Vehicle

采用自由滚转尾翼技术是解决鸭式布局导弹横滚控制的有效途径,针对某试飞器助推飞行段需求,设计了一型滚转尾翼。试验结果表明,滚转尾翼设计合理,性能良好,成功用于飞行试验。

Using free rolling tail is an effective way to solve the problem of rolling control for canardconfiguration missiles. Aiming at the mission requirements of some test vehicle in the boost flight phase,the design of type-one rolling tail was carried out,and the related test researches were completed at here.The results show that the rolling tail was a reasonable design,and with excellent performances,it was also successfully used in the flight test.