Long-range energy-state maneuvers for minimum time to specified terminal conditions

Author:

Parsons M. G.,Bryson A. E.,Hoffman W. C.

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Management Science and Operations Research,Control and Optimization

Reference7 articles.

1. Bryson, A. E., Jr., Desai, M. N., andHoffman, W. C.,Energy-State Approximation in Performance Optimization of Supersonic Aircraft, Journal of Aircraft, Vol. 6, No. 6, 1969.

2. Hedrick, J. K., andBryson, A. E., Jr.,Three-Dimensional, Minimum-Time Turns for a Supersonic Aircraft, Journal of Aircraft, Vol. 9, No. 2, 1972.

3. Parsons, M. G., andBryson, A. E., Jr.,Three-Dimensional, Minimum-Time Flight Paths to a Point and onto a Line for a Supersonic Aircraft with a Maximum Mach Number Constraint, Paper No. 32-4, Joint Automatic Control Conference, Stanford University, Stanford, California, 1972.

4. Kelley, H. J., andLefton, L.,Supersonic Aircraft Energy Turns, Paper Presented at the Fifth IFAC Congress, Paris, France, 1972.

5. Parsons, M. G.,Three-Dimensional, Minimum-Time Turns to a Point and onto a Line for a Supersonic Aircraft with a Maximum Mach Number Constraint, PhD Dissertation, Department of Applied Mechanics, Stanford University, Stanford, California, 1972.

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