Optimal Thrust and Aerodynamic Controls in Hypersonic Flight

摘要: The general equations of motion for a thrusting, lifting vehicle flying inside non rotating planetary atmosphere with central gravitational force field are presented in vector form. It is shown that the optimal thrust and aerodynamic controls governed by Lawden’s primer \( {\bar p_\nu } \), adjoint associated velocity vector. control laws integrals derived For case where used at an intermediate level such as prolonged thrusting flight atmosphere, additional relations explicit expression modulated magnitude on this sustained arc obtained. Finally, using canonical transformation, two sets state together resulting obtained terms usual trajectory variables (r, θ, Φ, V, γ, ψ) employed hypersonic flight.