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目前对航天器共振轨道特性的研究还非常不完善。为此,对频率为0.5的航天器典型共振轨道理论进行了补充,分析了共振轨道的参数转换模式,提出了共振轨道物理平面方程的直接参数描述方法。对单段共振轨道机动在典型任务中的应用进行了仿真分析,分析对比了共振轨道机动与传统轨道机动的优缺点。同时,通过仿真计算,对共振轨道周期特性进行了研究。研究发现,共振轨道等效速度增量是随时间尺度参数的改变进行准周期变化,而并非严格的周期变化,这一点与文献[3]中的研究结果有所不同。
At present, the research on spacecraft resonance orbit characteristics is still not perfect. To this end, the typical resonance orbit theory of the spacecraft with a frequency of 0.5 is supplemented, and the parameter conversion mode of the resonance orbit is analyzed. A direct parameter description method of the resonance orbit physical plane equation is proposed. The application of the single-section resonance orbit maneuver in typical missions is simulated and analyzed, and the advantages and disadvantages of the resonance orbit maneuver and the traditional orbit maneuver are analyzed and compared. At the same time, the periodic orbit characteristics of the resonant orbit have been studied through simulation. The study found that the equivalent orbital velocity increment of the resonance orbitals varies quasi-periodically with the change of the time-scale parameters, rather than strictly periodic changes, which is different from the results in [3].