针对观测站机动前目标距离未知导致无法计算Fisher信息矩阵(Fisher information matrix,FIM)的问题,从粗估目标初始距离和减小粗估误差对FIM行列式影响两方面着手,提出在转向前计算FIM进而设计机动策略的方法。首先,在修正极坐标系下建...针对观测站机动前目标距离未知导致无法计算Fisher信息矩阵(Fisher information matrix,FIM)的问题,从粗估目标初始距离和减小粗估误差对FIM行列式影响两方面着手,提出在转向前计算FIM进而设计机动策略的方法。首先,在修正极坐标系下建立系统模型,描述了观测站leg-by-leg机动模式下FIM的计算方法。其次,通过假设目标速度实现目标初始状态粗估,提出使归一化初始距离粗估误差最小的目标速度假设方法。然后,对FIM行列式进行近似及多项式展开,通过控制前后leg段比例以减小状态粗估误差对FIM行列式的影响。最后,利用仿真验证了所提机动策略设计方法的可行性和有效性。结果表明,对于典型的水下目标跟踪场景,FIM行列式的有效估计概率为76.7%,平均的相对估计误差为0.12。展开更多
在轨服务飞行器(Orbital Service Vehicle,OSV)在执行服务任务时,可以采取多种方案和策略接近服务目标。为得到优化可行的机动策略,可以运用适当的指标体系和评估算法对各方案进行统一比较和选优。根据效能评估的相关理论,提出了基于改...在轨服务飞行器(Orbital Service Vehicle,OSV)在执行服务任务时,可以采取多种方案和策略接近服务目标。为得到优化可行的机动策略,可以运用适当的指标体系和评估算法对各方案进行统一比较和选优。根据效能评估的相关理论,提出了基于改进的层次分析法的OSV机动策略评估方法,并用具体算例验证了该方法的可行性和可信性。该方法经过适当的细化可以推广应用于其它航天任务的决策过程中。展开更多
To design the terminal maneuver strategy of an anti-ship missile,first,the analytical solution of miss distance when an anti-ship missile has planar weaving maneuver and three-dimension spiral maneuver is presented,in...To design the terminal maneuver strategy of an anti-ship missile,first,the analytical solution of miss distance when an anti-ship missile has planar weaving maneuver and three-dimension spiral maneuver is presented,in which not only the amplitude and frequency are considered but also the initial phase is taken into account.Next,based on the analytical solution of miss distance,the effects on the miss distance of the amplitude,frequency,initial phase of the anti-ship missile＇s maneuver acceleration and the order of flight control system of the air-ship missile are analyzed.Finally,the optimum weaving maneuver and spiral maneuver which make the miss distance be the largest under some conditions are designed,which is of important meaning for increasing the survival probability of the anti-ship missile.展开更多
文摘针对观测站机动前目标距离未知导致无法计算Fisher信息矩阵(Fisher information matrix,FIM)的问题,从粗估目标初始距离和减小粗估误差对FIM行列式影响两方面着手,提出在转向前计算FIM进而设计机动策略的方法。首先,在修正极坐标系下建立系统模型,描述了观测站leg-by-leg机动模式下FIM的计算方法。其次,通过假设目标速度实现目标初始状态粗估,提出使归一化初始距离粗估误差最小的目标速度假设方法。然后,对FIM行列式进行近似及多项式展开,通过控制前后leg段比例以减小状态粗估误差对FIM行列式的影响。最后,利用仿真验证了所提机动策略设计方法的可行性和有效性。结果表明,对于典型的水下目标跟踪场景,FIM行列式的有效估计概率为76.7%,平均的相对估计误差为0.12。
文摘在轨服务飞行器(Orbital Service Vehicle,OSV)在执行服务任务时,可以采取多种方案和策略接近服务目标。为得到优化可行的机动策略,可以运用适当的指标体系和评估算法对各方案进行统一比较和选优。根据效能评估的相关理论,提出了基于改进的层次分析法的OSV机动策略评估方法,并用具体算例验证了该方法的可行性和可信性。该方法经过适当的细化可以推广应用于其它航天任务的决策过程中。
基金Supported by the Ministerial Level Advanced Research Foundation(0528)
文摘To design the terminal maneuver strategy of an anti-ship missile,first,the analytical solution of miss distance when an anti-ship missile has planar weaving maneuver and three-dimension spiral maneuver is presented,in which not only the amplitude and frequency are considered but also the initial phase is taken into account.Next,based on the analytical solution of miss distance,the effects on the miss distance of the amplitude,frequency,initial phase of the anti-ship missile＇s maneuver acceleration and the order of flight control system of the air-ship missile are analyzed.Finally,the optimum weaving maneuver and spiral maneuver which make the miss distance be the largest under some conditions are designed,which is of important meaning for increasing the survival probability of the anti-ship missile.
