An optimal terminal guidance method for continuous powered space vehicles.

Error correcting problem in space trajectory of continuous powered space vehicle, discussing optimal terminal guidance

[1]  R. E. Kalman,et al.  Controllability of linear dynamical systems , 1963 .

[2]  C. G. Pfeiffer,et al.  A technique for optimal final value control of powered flight trajectories. , 1966 .

[3]  R. Penrose.  On best approximate solutions of linear matrix equations , 1956, Mathematical Proceedings of the Cambridge Philosophical Society.

[4]  A. Woods.  The anomaly of convex bodies , 1956, Mathematical Proceedings of the Cambridge Philosophical Society.

[5]  J. Potter,et al.  A guidance-navigation separation theorem , 1964 .