The concept of pseudo-zero-effort-intercept is used in the proposed guidance to avoid thrust orientation break at the shift of the two guidance processes.
利用拟零控拦截概念使两个导引阶段平缓过渡,避免了导引方法切换时推力方向的跳变。
The concept of pseudo-zero-effort-intercept is used in the proposed guidance to avoid thrust orientation break at the shift of the two guidance processes.
利用拟零控拦截概念使两个导引阶段平缓过渡,避免了导引方法切换时推力方向的跳变。
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