Mars Powered Descent Trajectory Planning Method Based on Vector Trajectory
A trajectory planning, vector trajectory technology, applied in the field of deep space exploration
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[0099] In order to better illustrate the purpose and advantages of the present invention, the content of the invention will be further described below in conjunction with an embodiment and corresponding drawings.
[0100] like figure 1 As shown, the Mars dynamic descent trajectory planning method based on the vector trajectory disclosed in this embodiment, the specific implementation steps are as follows:
[0101] Step 1. Determine the dynamic equation of the Mars power descent section, the optimal performance index of fuel consumption and the constraint conditions.
[0102] The dynamic equation of Mars power descent section is shown in formula (34).
[0103]
[0104] Among them, x and z are the horizontal position and height of the lander respectively, and v x and v z are the speeds of the lander along the horizontal direction and the height direction, respectively, a x and a z are the accelerations of the lander along the horizontal direction and the height direction...
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