Effort was directed toward the problems of the real time trajectory optimization and guidance law development for the National Aerospace Plane (NASP) applications. In particular, singular perturbation methods were used to develop guidance algorithms suitable for onboard, real time implementation. The progress made in this research effort is reported.
Rapid near-optimal aerospace plane trajectory generation and guidance
1991-11-01
Report
No indication
English
Optimal Ascent Trajectory and Guidance Law for Aerospace Plane
British Library Conference Proceedings | 1999
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