Study on TT&C resources scheduling technique based on inter-satellite link

The navigation constellation will have the capability of supporting Tracking Telemetry and Command (TT&C) operations by inter-satellite link (ISL). The ISL will become an important solution to reduce the shortage of ground TT&C resources. The problems need to be studied urgently in the field of space TT&C network resources scheduling management are how to determine the availability of ISL and how to allocate TT&C resources of ISL. The performance and scheduling constraints of navigation constellation?s ISL are analyzed, and three utilization strategies of ISL to perform TT&C operations are proposed. The allocation of TT&C resources based on ISL falls into two successive phases. Firstly, master satellite determination equation is established by using 0–1 Programming model based on the availability matrix. Mathematical method is used to solve the equation to determine the master satellite and the topology of ISL. Secondly, Constraint Programming (CP) model is used to describe the ground TT&C resources scheduling problem with special requirements of TT&C operations based on master satellite, and a heuristic algorithm is designed to solve the CP model. The equations and algorithm are verified by simulation examples. The algorithm of TT&C resources scheduling based on ISL has realized the synthesized usage of both the ISL and ground resources on TT&C field. This algorithm can improve TT&C supports of territorial ground TT&C network for global navigation constellation, and provides technical reference for the TT&C mission planning of global constellation by using ISL.     

航天器贮箱大幅液体晃动三维质心面等效模型研究

针对航天器贮箱内的大幅液体晃动建立了三维质心面等效模型,此模型将贮箱内液体等效为位于液体质心处的质点,该质心点可以在质心约束面内任意运动,同时利用质心点动力学方程及接触碰撞模型近似计算液体晃动对贮箱的作用力。质心面等效模型的数值仿真结果与基于VOF方法的流体动力学数值计算结果基本吻合,从而验证了质心面等效模型用于航天器贮箱大幅液体晃动分析的有效性。     

带作用力约束的二维装填布局问题--航天器中复杂插座板上插孔的布局优化设计

研究航天器中一种复杂插座板上插孔的布局设计问题 ,简化为在圆形插板上 ,根据给定的 n个插头 ,考虑插座板的非凸的可布空间和插头的拔脱力、插座板的紧固螺栓力、边缘弹簧的弹簧力等约束情况下 ,布置其插孔位置。它属于带作用力约束的二维装填 ( Packing)问题。给出该问题的数学模型 ,并提出一种改进编码的遗传算法进行求解。文后附以航天器复杂插座上插孔布局设计实际工程问题为背景的算例     

深空探测器约束简化与任务规划方法研究

针对深空探测器现有的任务规划方法在处理系统间复杂约束时存在的约束复杂度高、实时响应能力差、计算效率低等问题,提出一种新的约束简化方法和启发式连续任务规划方法。首先,在时间线规划模型中根据两两子系统间的实时状态关系定义启发式因子,并利用该因子在规划周期内的取值建立子系统间时间线临时从属关系,从而合理地降低规划过程中的约束复杂程度;然后,在规划算法中采用时间线状态扩展策略,根据时间线临时从属关系对各子系统间的状态进行横向和纵向扩展,从而实现对目标任务规划进行快速排序。仿真结果表明由启发式因子建立的时间线临时从属关系有效简化了任务规划过程中的时间约束和资源约束、提高了任务规划的效率和灵活性。