Multistage Trajectory Optimization with Radar Range Constraints

The problem of finding an optimal aircraft trajectory for long-distance flights in three dimensions subject to radar detection constraints is considered. A general point-mass model previously developed is not suitable because the time discretization needs to be very fine to resolve the rigid-body dynamics resulting in very large optimization problems. Different reduced mathematical models are derived and compared to the more general performance model. Finally, a long-range mission involving two subsonic jet trainers approaching a radar target is numerically simulated. The results indicate that the time a hostile radar has an approaching aircraft under surveillance can be greatly reduced by using the proposed methodology.

[1]  Martin Norsell,et al.  Radar cross section constraints in flight-path optimization , 2003 .

[2]  Ulf Ringertz Aircraft Trajectory Optimization as a Wireless Internet Application , 2004, J. Aerosp. Comput. Inf. Commun..

[3]  Ulf Ringertz,et al.  Optimal Trajectory for a Minimum Fuel Turn , 2000 .

[4]  John Paterson,et al.  Overview of Low Observable Technology and Its Effects on Combat Aircraft Survivability , 1999 .

[5]  Martin Norsell,et al.  Aircraft trajectories considering radar range constraints , 2002 .

[6]  J. T. Betts Experience with a Sparse Nonlinear Programming Algorithm , 1997 .

[7]  Bernard Etkin,et al.  Dynamics of flight , 1959 .

[8]  S. M. Shahruz,et al.  Formation of a group of unmanned aerial vehicles (UAVs) , 2001, Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148).

[9]  P. Gill,et al.  Large-scale SQP methods and their application in trajectory optimization , 1994 .

[10]  Phillip R. Chandler,et al.  UAV cooperative control , 2001, Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148).

[11]  Scott A. Bortoff,et al.  Path planning for UAVs , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).

[12]  Ulf Ringertz,et al.  Flight testing an optimal trajectory for the Saab J35 Draken , 2000 .

[13]  Richard M. Murray,et al.  Low-observable nonlinear trajectory generation for unmanned air vehicles , 2003, 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475).

[14]  C. Hargraves,et al.  DIRECT TRAJECTORY OPTIMIZATION USING NONLINEAR PROGRAMMING AND COLLOCATION , 1987 .

[15]  J. Betts Survey of Numerical Methods for Trajectory Optimization , 1998 .

[16]  D. C. Jenn,et al.  Radar and laser cross section engineering , 2005 .

[17]  Martin Norsell,et al.  Flight Testing Radar Detection of the Saab 105 in Level Flight , 2002 .

[18]  C. D. Boor,et al.  Package for calculating B-splines , 1977 .