A low-orbit constellation deployment method based on Mars atmospheric assistance
A low-orbit constellation and atmospheric technology, applied in the aerospace field, can solve problems such as the deployment of multiple aircraft that are not given
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[0104] like figure 2 As shown, a low-orbit constellation deployment method based on Mars atmosphere assistance disclosed in this embodiment includes the following steps:
[0105] Step 1: Establish the motion equation of the probe in the Martian equatorial inertial coordinate system, determine the number of orbital elements of the probe, and then determine the position of the far fire point of the probe. The probe carries multiple constellation vehicles that require low-orbit constellation deployment. The number of spacecraft carrying the constellation depends on the requirements of the constellation mission.
[0106] Step 1.1: Establish the motion equation of the probe under the Martian equatorial inertial coordinate system;
[0107] like figure 2 As shown, choose the center of mass of Mars as the origin to establish the equatorial inertial coordinate system, choose the X-axis to be within the equator of the planet and point to the vernal equinox, the Z-axis points to the...
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