Cooperative Interception with Double-Line-of-Sight-Measuring

Estimation and guidance scheme is presented, which enables two missiles tracking single target cooperatively. Each missile is equipped with an infra-red sensor and measures the LOS angle only. The two missiles form a measuring baseline relative to the target in space and share measured information with each other, enabling that each identies the target state based triangulation method. However, the observability of this double line-ofsight measuring relative navigation method is weak if the separation angle between both line-of-sight vectors is small. This paper proposes a guidance law that modulates the lineof-sight angle through a performance index. Using this guidance law, the missile with large initial ling-of-sight angle maximizes this index. Whereas the other one minimizes it. Simulation results show that the proposed estimation and guidance scheme improves the homing accuracy and can yield hit-to-kill performance.

[1]  Shijie Xu,et al.  Approach Guidance with Double-Line-of-Sight Measuring Navigation Constraint for Autonomous Rendezvous , 2011 .

[2]  Yaakov Oshman,et al.  Cooperative Interception in a Multi-Missile Engagement , 2009 .

[3]  R. Singer Estimating Optimal Tracking Filter Performance for Manned Maneuvering Targets , 1970, IEEE Transactions on Aerospace and Electronic Systems.

[4]  Yaakov Oshman,et al.  Optimal observer trajectories for passive target localization using bearing-only measurements , 1996 .

[5]  Josef Shinar,et al.  Decision-Directed Adaptive Estimation and Guidance for an Interception Endgame , 2006 .

[6]  Jason L. Speyer,et al.  Maximum-information guidance for homing missiles , 1984 .

[7]  Shijie Xu,et al.  Double line-of-sight measuring relative navigation for spacecraft autonomous rendezvous☆ , 2010 .

[8]  K. Gong,et al.  Fundamental properties and performance of conventional bearings-only target motion analysis , 1984 .

[9]  Paul Zarchan,et al.  Kill Vehicle Guidance and Control Sizing For Boost-Phase Intercept , 2011 .

[10]  Paul Zarchan,et al.  Tactical and strategic missile guidance , 1990 .

[11]  Josef Shinar,et al.  ON THE VALIDITY OF LINEARIZED ANALYSIS IN THE INTERCEPTION OF REENTRY VEHICLES , 1998 .

[12]  Paul Zarchan,et al.  Fundamentals of Kalman Filtering: A Practical Approach , 2001 .

[13]  Paul Zarchan Representation of Realistic Evasive Maneuvers by the Use of Shaping Filters , 1979 .

[14]  Jeremy A. Hodgson,et al.  Trajectory Optimization Using Differential Inclusion to Minimize Uncertainty in Target Location Estimation , 2005 .

[15]  Naiming Qi,et al.  Linear Quadratic Differential Game Strategies with Two-pursuit Versus Single-evader , 2012 .

[16]  Jason L. Speyer,et al.  Estimation enhancement by trajectory modulation for homing missiles , 1984 .