... fuel compartment ==> 燃料舱,燃油舱 fuel constraints ==> 燃料制约 fuel consumption ==> 燃料消耗=>燃料消费量 ...
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Furthermore, an attainable set for initial conditions of the gravity-turn descent is deduced according to the constraints of thrust, fuel and states of the soft landing system.
此外,根据软着陆系统推力、燃料和状态的约束条件,给出了引力转弯着陆过程初始条件的可达集合。
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.
算法能够以较省的燃料消耗实现轨道面内任意方向、任意时间内满足约束的近距离交会。
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