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Pursuit-evasion game theoretic uncertainty oriented sensor management for elusive space objects

机译:追求逃避游戏理论不确定性的难以实现空间物体的传感器管理

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A pursuit-evasion (PE) orbital game approach for space situational awareness (SSA) is presented to deal with imperfect measurements and informational uncertainties. In the two-sided optimization problem, a pursuer (an observer or sensor) will use the sensor resource to minimize the uncertainty (modeled by entropy) while an evader (a space object being tracked) will maximize it by performing space maneuvers. Since the cost and opportunity cost of sensor resources, pursuer will make decisions on the when to use these resources. The proposed PE approach provides a method to solve the SSA problem, where the evader will exploit the sensing and tracking model to confuse the opponent by corrupting their tracking estimates, while the pursuer wants to efficiently decrease the tracking uncertainties. A numerical simulation scenario with one space based space surveillance (SBSS) satellite as a pursuer and one geosynchronous (GEO) satellite as an evader is simulated to demonstrate the PE orbital game approach. The GEO applies the continuous low-thrust such as the Ion thrust in maneuvers. An add-on module is developed for SGP4/SDP4 algorithms to propagate the satellites with maneuvers. The GEO maneuvering strategies and on-off measurement controls for SBSS are obtained from the Nash equilibrium of the PE game.
机译:追求逃守(PE)空间情境意识(SSA)的轨道游戏方法是为了应对不完美的测量和信息性不确定性。在双面优化问题中,追求者(观察者或传感器)将使用传感器资源来最小化不确定性(由熵建模),而避难所(被跟踪的空间对象)将通过执行空间操纵来最大化它。由于传感器资源的成本和机会成本,追求者将在使用这些资源时作出决策。所提出的PE方法提供了一种解决SSA问题的方法,其中避难者将利用传感和跟踪模型来通过损坏他们的跟踪估计来混淆对手,而追求者希望有效地降低跟踪不确定性。模拟了一个基于空间的空间监控(SBSS)卫星的数值模拟场景作为追捕者和一个地球同步(Geo)卫星作为避难者,以展示PE轨道游戏方法。地理施加连续的低推力,例如机动中的离子推力。为SGP4 / SDP4算法开发了一个附加模块,以将卫星与机动传播。 SBSS的Geo机动策略和开关测量控制是从PE PE游戏的纳什平衡获得的。

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