Estimation Enhancement by Cooperatively Imposing Relative Intercept Angles
暂无分享,去创建一个
[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 .