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Potential applications of skip SMV with thrust engine

机译:带推力发动机的跳跃式SMV的潜在应用

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This paper investigates the potential applications of Space Maneuver Vehicles (SMV) with skip trajectory. Due to soaring space operations over the past decades, the risk of space debris has considerably increased such as collision risks with space asset, human property on ground and even aviation. Many active debris removal methods have been investigated and in this paper, a debris remediation method is first proposed based on skip SMV. The key point is to perform controlled re-entry. These vehicles are expected to achieve a trans-atmospheric maneuver with thrust engine. If debris is released at altitude below 80 km, debris could be captured by the atmosphere drag force and re-entry interface prediction accuracy is improved. Moreover if the debris is released in a cargo at a much lower altitude, this technique protects high value space asset from break up by the atmosphere and improves landing accuracy. To demonstrate the feasibility of this concept, the present paper presents the simulation results for two specific mission profiles: descent to predetermined altitude; descent to predetermined point (altitude, longitude and latitude). The evolutionary collocation method is adopted for skip trajectory optimization due to its global optimality and high-accuracy. This method is actually a two-step optimization approach based on the heuristic algorithm and the collocation method. The optimal-control problem is transformed into a nonlinear programming problem (NLP) which can be efficiently and accurately solved by the sequential quadratic programming (SQP) procedure. However, such a method is sensitive to initial values. To reduce the sensitivity problem, genetic algorithm (GA) is adopted to refine the grids and provide near optimum initial values. By comparing the simulation data from different scenarios, it is found that skip SMV is feasible in active debris removal and the evolutionary collocation method gives a truthful re-entry trajectory that satisfies the path and boundary constraints.
机译:本文研究具有跳跃轨迹的太空机动车辆(SMV)的潜在应用。由于过去几十年来飞速发展的太空活动,太空碎片的风险大大增加,例如与太空资产,地面人员甚至航空的碰撞风险。已经研究了许多主动清除碎片的方法,并且本文首次提出了基于跳过SMV的碎片修复方法。关键是执行受控重入。预计这些车辆将通过推力发动机实现跨大气机动。如果在80 km以下的高度释放碎片,则大气阻力可以捕获碎片,从而提高了重入界面的预测精度。此外,如果碎片以较低的高度释放在货物中,则该技术可以保护高价值的太空资产免遭大气破坏,并提高着陆精度。为了证明这一概念的可行性,本文提出了两种具体任务的仿真结果:下降到预定高度;下降到预定点(海拔,经度和纬度)。由于其全局最优性和高精度,因此采用进化搭配方法进行跳跃轨迹优化。该方法实际上是基于启发式算法和搭配方法的两步优化方法。最优控制问题被转化为非线性规划问题(NLP),可以通过顺序二次规划(SQP)程序有效而准确地解决该问题。但是,这种方法对初始值敏感。为了减少灵敏度问题,采用遗传算法(GA)改进网格并提供接近最佳的初始值。通过比较来自不同场景的模拟数据,发现跳过SMV在主动碎片清除中是可行的,并且进化配置方法给出了满足路径和边界约束的真实的重入轨迹。

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