Practical guidance for homing missiles with bearings-only measurements

Observability is analyzed for the target tracking with bearings-only measurements (BOM) applied to a passive homing missile system using augmented proportional navigation guidance (APNG). Based on the analysis, a practical homing guidance law is proposed to enhance observability for tactical missile applications. The new guidance law is tailored to provide oscillation of line-of-sight (LOS) angle induced by initial missile heading errors without sacrificing terminal effectiveness. Simulation studies indicate that the proposed guidance law provides convergence of the state estimates essential to homing guidance applications as well as terminal effectiveness.

[1]  J. Speyer,et al.  Comparison of several extended Kalman filter formulations for homing missile guidance , 1980 .

[2]  V. Aidala Kalman Filter Behavior in Bearings-Only Tracking Applications , 1979, IEEE Transactions on Aerospace and Electronic Systems.

[3]  J. Speyer,et al.  A stochastic analysis of a modified gain extended Kalman filter with applications to estimation with bearings only measurements , 1983, The 22nd IEEE Conference on Decision and Control.

[4]  W. Grossman Bearings-only tracking - A hybrid coordinate system approach , 1994 .

[5]  M. Gavish,et al.  Nth-order dynamics target observability from angle measurements , 1988 .

[6]  D. Hull,et al.  Linear-quadratic guidance law for dual control of homing missiles , 1990 .

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

[8]  Paul Zarchan,et al.  A New Look at Classical vs Modern Homing Missile Guidance , 1981 .

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

[10]  Arthur E. Bryson,et al.  Applied Optimal Control , 1969 .

[11]  Min-Jea Tahk,et al.  Use of Intermittent Maneuvers for Miss Distance Reduction in Exoatmospheric Engagements , 1989 .

[12]  Jason L. Speyer,et al.  Performance of the modified-gain extended Kalman filter along an enhanced information path of a homing missile , 1986 .

[13]  S. N. Balakrishnan,et al.  Coordinate-transformation-based filter for improved target tracking , 1986 .

[14]  Richard James Casler Dual-Control Guidance Strategy for Homing Interceptors Taking Angle-Only Measurements , 1978 .

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

[16]  V. Aidala,et al.  Biased Estimation Properties of the Pseudolinear Tracking Filter , 1982, IEEE Transactions on Aerospace and Electronic Systems.

[17]  V. Aidala,et al.  Utilization of modified polar coordinates for bearings-only tracking , 1983 .

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

[19]  David V. Stallard,et al.  Angle-only tracking filter in modified spherical coordinates , 1991 .

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

[21]  Sherry Hammel,et al.  Observability Requirements for Three-Dimensional Tracking via Angle Measurements , 1985, IEEE Transactions on Aerospace and Electronic Systems.

[22]  David V. Stallard AN ANGLE-ONLY TRACKING FILTER FOR A MANEUVERING TARGET , 1990 .