Design and optimization of homing trajectory is essential for accurate aerial delivery of parafoil system.
归航轨迹的设计和优化对实现翼伞系统的精确空投至关重要。
In order to realize accurate and safe landing of parafoil system, classic multiphase homing trajectory was adopted according to the maneuverability and basic flight characters of the parafoil itself.
为了实现翼伞系统的准确、安全着陆，根据翼伞系统自身的可操纵性和基本运动特性，采用经典分段归航策略。
The computation equation and design criterion of real effective navigation ratio of homing control trajectory in PN homing guidance system were given.
给出了PN寻的制导系统的控制弹道实际有效导航比的计算公式及设计准则。
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