科技报告详细信息
High-Fidelity Multiple-Flyby Trajectory Optimization Using Multiple-Shooting
Ellison, Donald H ; Englander, Jacob A
关键词: FLYBY MISSIONS;    SWINGBY TECHNIQUE;    SPACECRAFT TRAJECTORIES;    TRAJECTORY OPTIMIZATION;    ACCURACY;    NONLINEAR PROGRAMMING;    NUMERICAL INTEGRATION;   
RP-ID  :  GSFC-E-DAA-TN71688
学科分类:天文学(综合)
美国|英语
来源: NASA Technical Reports Server
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【 摘 要 】

Rendering a complex spacecraft trajectory in high fidelity can be an expensive endeavor, both computationally and from a human time/cost standpoint. However, in many cases, a low-fidelity trajectory that reasonably approximates a high-fidelity counterpart is much easier to obtain. Thus, it is important to have an efficient process for converting a trajectory from lower-fidelity model to high fidelity. We present a method for converting low-fidelity trajectories into high fidelity that relies on multiple shooting, nonlinear programming, and numerical integration. The procedure converts any zero-radius sphere-of-influence gravity-assist events to fully integrated flyby events. Several numerical examples are presented that showcase the flexibility of the high-fidelity rendering process across multiple mission types and flight regimes.

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