rendezvous guidance

基本解釋

This paper presents the approaches and practical theoretical models on synthetic orbit maneuver during long distance guidance stage of space rendezvous.
文章研究了空間交會(huì)遠(yuǎn)程導(dǎo)引階段綜合變軌問題的變軌策略方法和實(shí)用理論模型。
The other scenarios illustrate that the guidance algorithm can ensure a close range rendezvous motion in any direction, at any time with the fuel economy and under the constraints as well.
算法能夠以較省的燃料消耗實(shí)現(xiàn)軌道面內(nèi)任意方向、任意時(shí)間內(nèi)滿足約束的近距離交會(huì)。
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The structural form of three kinds of optimum rendezvous guidance laws are presented. Simultaneously the equations of parameters depended an optimum rendezvous guidance laws of three kinds are given.
除給出了最優(yōu)交會(huì)體制導(dǎo)律的結(jié)構(gòu)形式外，還提供了求解最優(yōu)交會(huì)制導(dǎo)律的參數(shù)方程組。