在飞行初段,提出用直接力来对弹道进行调姿以减小中制导段需用过载的方案,并利用最优控制的方法设计了直接力作用方案。
During the initial flight phase, the method which regulates the ballistic trajectory to reduce the overload requirement of the flight middle phase using the direct force is presented.
在飞行初段,提出用直接力来对弹道进行调姿以减小中制导段需用过载的方案,并利用最优控制的方法设计了直接力作用方案。
During the initial flight phase, the method which regulates the ballistic trajectory to reduce the overload requirement of the flight middle phase using the direct force is presented.
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