论文信息 - General Variational Theory of the Flight Paths of Rocket-Powered Aircraft, Missiles and Satellite Carriers

General Variational Theory of the Flight Paths of Rocket-Powered Aircraft, Missiles and Satellite Carriers

General equations are presented for analyzing the optimum flight paths of rocket-powered aircraft, missiles and satellites. The Earth is assumed spherical; the variability of the acceleration of gravity with the altitude is accounted for.

Angelo Miele

[1] Angelo Miele,et al. Optimum Climbing Technique for a Rocket-Powered Aircraft , 1955 .

[2] Burton D. Fried,et al. Optimum Rocket Trajectories , 1956 .

[3] Angelo Miele. An Extension of the Theory of the Optimum Burning Program for the Level Flight of a Rocket-Powered Aircraft , 1957 .

[4] Angelo Miele,et al. Generalized Theory of the Optimum Thrust Programming for the Level Flight of a Rocket-Powered Aircraft , 1956 .

[5] J. Breakwell. The Optimization of Trajectories , 1959 .

[6] Angelo Miele. On the Brachistochronic Thrust Program for a Rocket Powered Missile Traveling in an Isothermal Medium , 1958 .

[7] A. E. Bryson,et al. Optimum Rocket Trajectories With Aerodynamic Drag , 1958 .