The multi-impulse glideslope guidance algorithm for close range rendezvous of spacecraft is presented.
提出了满足测量视场、最小脉冲间隔、最大脉冲受限等约束的燃料最省的航天器近距离交会多脉冲斜滑制导算法。
Rapid frequency acquisition and tracking for pilot pulse carrier;
导频脉冲载波频率的快速捕获与跟踪
