Integrated Design of Fast Access Regressive Orbit and Maneuver Launch Position

Inhalt:
Based on the orbit dynamics and spherical geometry principles, the design models of fast access regressive orbit and maneuver launch position are built for the typical mission of operationally responsive recursive orbit by road-based maneuver launch. Considering the requirement of operationally responsive space, the relationship between orbit parameters and launch position is established with the variable of maneuver launch site and the optimization goal of response time. Then the integrated design method of fast access regressive orbit and maneuver launch position in an enclosed area is reached. For a concrete example, the optimized orbit parameters and maneuver launch site corresponding to the shortest orbit response time and task response time are accomplished by the method. STK is successfully used to simulate the planning results with the shortest task response time, demonstrating the feasibility and practicability of the method. The relevant design method can provide theoretical support for the design of operationally responsive orbit and maneuver launch site.