Determining method for terminal guidance shift-exchange conditions of reenter vehicle
A technology for re-entry aircraft and determination method, which is applied in the field of determining the terminal guidance shift conditions of re-entry aircraft, and achieves the effects of enhancing robustness, improving fault tolerance, and reducing command hardware limits
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[0026] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.
[0027] Such as figure 1 As shown, the present invention relates to a method for determining the handover condition of the terminal guidance of a reentry vehicle, and the specific steps are as follows:
[0028] 1. Generate preset shift points;
[0029] Such as figure 2 As shown in , set the reentry constraint boundary (heat flow, overload, dynamic pressure, etc.) through the given reentry point information (including position, velocity, velocity inclination and attitude) and strike target information (target position, velocity), Through the simulation planning, the longitudinal profile of the re-entry vehicle is generated, and the preset handover point information that meets the flight requirements is initially obtained.
[0030] The planning of the reentry trajectory can adopt the commonly used reentry trajectory optimization algorithm based on the ...
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