Estimation Enhancement by Cooperatively Imposing Relative Intercept Angles

Cooperative estimation/guidance for a team of missiles is the topic of this paper. An example scenario is considered where an aircraft simultaneously launches several cooperative defending missiles as a countermeasure against an attacking homing missile. A new reduced-order estimation scheme based on information sharing to cooperatively estimate the relative states and the unknown parameters of the attacking missile is proposed. Each defending missile shares its own noise-corrupted line-of-sight angle measurement with the rest of the team. The observability of this multi-line-of-sight measuring environment is enhanced by cooperatively imposing nonnegative relative intercept angles between consecutive defenders. The ability of the proposed strategy to protect the targeted aircraft is studied for a two-defender case via extensive Monte Carlo simulations. The effect of different values of the commanded relative intercept angle on the pure estimation as well as on the intertwined guidance-estimation performan...

[1]  Alexander Zhurbal,et al.  Effect of Estimation on the Performance of an Integrated Missile Guidance and Control System , 2011, IEEE Transactions on Aerospace and Electronic Systems.

[2]  Eloy Garcia,et al.  Cooperative Strategies for Optimal Aircraft Defense from an Attacking Missile , 2015 .

[3]  Tal Shima,et al.  Cooperative Optimal Guidance Laws for Imposing a Relative Intercept Angle , 2015 .

[4]  J. Shinar,et al.  A discrete dynamic game modelling anti-missile defense scenarios , 1995 .

[5]  Min-Jea Tahk,et al.  Time-to-go weighted optimal guidance with impact angle constraints , 2006, IEEE Transactions on Control Systems Technology.

[6]  R. G. Cottrell Optimal intercept guidance for short-range tactical missiles , 1971 .

[7]  Niket S. Kaisare,et al.  Incorporating delayed and infrequent measurements in Extended Kalman Filter based nonlinear state estimation , 2011 .

[8]  Roger Boyell,et al.  Defending a Moving Target Against Missile or Torpedo Attack , 1976, IEEE Transactions on Aerospace and Electronic Systems.

[9]  Tal Shima,et al.  Line-of-Sight Interceptor Guidance for Defending an Aircraft , 2011 .

[10]  Tal Shima,et al.  Optimal Cooperative Pursuit and Evasion Strategies Against a Homing Missile , 2011 .

[11]  V. Aidala,et al.  Observability Criteria for Bearings-Only Target Motion Analysis , 1981, IEEE Transactions on Aerospace and Electronic Systems.

[12]  Tal Shima,et al.  Linear Quadratic Optimal Cooperative Strategies for Active Aircraft Protection , 2012 .

[13]  Yanfang Liu,et al.  Cooperative Interception with Double-Line-of-Sight-Measuring , 2013 .

[14]  Y. Oshman,et al.  Optimization of observer trajectories for bearings-only target localization , 1999 .

[15]  N. A. Shneydor,et al.  Comments on "Defending a Moving Target Against Missile or Topedo Attack" , 1977 .

[16]  D. Joseph,et al.  On linear control theory , 1961, Transactions of the American Institute of Electrical Engineers, Part II: Applications and Industry.

[17]  Tal Shima,et al.  Cooperative Multiple-Model Adaptive Guidance for an Aircraft Defending Missile , 2010 .

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

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

[20]  T. Shima,et al.  Linear Quadratic Guidance Laws for Imposing a Terminal Intercept Angle , 2008 .

[21]  Roger Boyell,et al.  Counterweapon Aiming for Defense of a Moving Target , 1980, IEEE Transactions on Aerospace and Electronic Systems.

[22]  V. Garber Optimum intercept laws for accelerating targets. , 1968 .

[23]  R. Asher,et al.  Optimal Guidance with Maneuvering Targets , 1974 .

[24]  Luke Chia‐Liu Yuan,et al.  Homing and Navigational Courses of Automatic Target‐Seeking Devices , 1948 .

[25]  Paul Zarchan,et al.  Proportional navigation and weaving targets , 1995 .

[26]  H. Simon,et al.  Dynamic Programming Under Uncertainty with a Quadratic Criterion Function , 1956 .

[27]  Ernest J. Ohlmeyer Root-mean-square miss distance of proportional navigation missile against sinusoidal target , 1996 .

[28]  Min-Jea Tahk,et al.  Homing Guidance Law for Cooperative Attack of Multiple Missiles , 2010 .

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

[30]  Tal Shima,et al.  Cooperative Differential Games Strategies for Active Aircraft Protection from a Homing Missile , 2010 .

[31]  Tal Shima,et al.  Differential games missile guidance with bearings-only measurements , 2013, IEEE Transactions on Aerospace and Electronic Systems.

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

[33]  Tal Shima,et al.  Multiple Model Adaptive Evasion Against a Homing Missile , 2016 .

[34]  Stephan A. R. Hepner,et al.  Observability analysis for target maneuver estimation via bearing-only and bearing-rate-only measurements , 1990 .

[35]  Yaakov Oshman,et al.  Stochastic Cooperative Interception Using Information Sharing Based on Engagement Staggering , 2016 .

[36]  Takeshi Yamasaki,et al.  Modified Command to Line-of-Sight Intercept Guidance for Aircraft Defense , 2013 .

[37]  Min-Jea Tahk,et al.  Optimal Guidance Laws with Terminal Impact Angle Constraint , 2005 .

[38]  Shaul Gutman,et al.  Applied min-max approach to missile guidance and control , 2005 .

[39]  Tal Shima,et al.  Target Evasion from a Missile Performing Multiple Switches in Guidance Law , 2016 .

[40]  Iwao Sasase,et al.  Maneuver target tracking with an acceleration estimator using target past positions , 2002 .

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

[42]  Tal Shima,et al.  Estimation Enhancement by Imposing a Relative Intercept Angle for Defending Missiles , 2017 .

[43]  Amir Averbuch,et al.  Interacting Multiple Model Methods in Target Tracking: A Survey , 1988 .

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