Search method for multi-constrained earth-moon transfer orbit cluster with equal launch intervals
A technology of transfer orbit and search method, applied in the field of multi-constraint Earth-Moon transfer orbit cluster search for lunar exploration
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[0088] Below in conjunction with accompanying drawing, the present invention will be further described:
[0089] The whole search process of the present invention is as follows image 3 As shown, this embodiment includes the following steps:
[0090] Step 1: Determine the number N of Earth-Moon transfer orbits that need to be designed to meet the constraints 0 =5 and the transmission time interval T is 10min.
[0091] Step 2: Determine the boundary constraints and the corresponding orbit search convergence conditions, including perilunar point constraints, such as the perilunar point height h p =200km, near-moon point inclination i L =45°; perigee constraints, such as the launch date of the launch vehicle t 0 Take March 3, 2017, the adjustable range of the launch direction Adjustable range of free gliding time [t 1 ,t 2 ]=[100s,1000s]; orbit search convergence conditions, such as equal launch time interval search convergence interval ΔT=0.5min, perilunar point height s...
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