Optimum Maneuvers for Launching Satellites Into Circular Orbits of Arbitrary Radius and Inclination

Abstract

2 Miele, A., A Survey of the Problems of Optimizing Flight Paths of Aircraft and Missiles, ARS preprint 1219-60. 3 Breakwell, J. V., The Optimization of Trajectories, J. Soc. Indust. Appl. Math., vol. 7, no. 2, June 1959, pp. 215-247. 4 Kelley, H. J., Gradient Theory of Optimal Flight Paths, ARS preprint 1230-60. 5 Kulakowski, L. J. and Stancil, R. T., Boost Trajectories for Maximum Burn-Out Velocity, ARS JOURNAL, vol. 30, no. 7, July 1960, pp. 612-618. 6 Bliss. G. A., Lectures on the Calculus of Variations, University of Chicago Press, Chicago, First Ed., 1946, Chap. 7. 7 Cicala, C. and Miele, A., Brachistochronic Maneuvers of a Variable Mass Aircraft in a Vertical Plane, J. Aero. Sci., vol. 22, no. 8, Aug. 1955, pp. 577-578. 8 Wheelon, A. D., Free Flight of a Ballistic Missile, ARS JOURNAL, vol. 29, no. 12, Dec. 1959, pp. 915-926. 9 Leitmann, G., On a Class of Variational Problems in Rocket Flight, J. Aero/Space Sci., vol. 26, no. 9, 1959. 10 Leitmann, G., Minimum Transfer Time for a Power-Limited Rocket, XI Int. Astronautical Congress, Stockholm, 1960. 11 Fried, B. D., On the Powered Flight Trajectory of an Earth Satellite, J E T PROPULSION, vol. 27, no. 6, June 1957, pp. 641-643.