This paper presents the analytical solutions of the problem of optimum maneuvering of a glide vehicle flying in the hypervelocity regime. The investigation is based on the approximation of Allen and Eggers; namely, that along the fundamental part of a reentry or ascent trajectory, the aerodynamic forces greatly exceed the components of the gravitational force in the directions tangent and normal to the flight path.Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/45214/1/10957_2004_Article_BF00926526.pd
Abstract. Necessary conditions for minimax problems with isolated or flat maxima re presented. Some ...
Research results are presented of an investigation of the optimum maneuvers of advanced shuttle type...
[[abstract]]This paper presents the exact dimensionless equations of motion and the necessary condit...
Necessary conditions for minimax problems with isolated or flat maxima are presented. Some relevant ...
With the advent of aeroassist technology for orbital transfers, it is of interest to have explicit o...
A major problem with operations of lifting reentry vehicle having an aft center-of-gravity location ...
The aero-gravity assist maneuver is here proposed as a tool to improve the efficiency of the gravity...
This paper presents the optimal solu-tions to the maximum endurance subsonic by the application of P...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76170/1/AIAA-8575-707.pd
This paper considers the problem of optimizing the flight trajectory of a rocket vehicle moving in a...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76843/1/AIAA-1985-1817-421.pd
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
This paper presents the necessary conditions for solving Chebyshev minimax (or maximax) problems wit...
Control programs and flight paths of a hypersonic vehicle in climb are analyzed. Two approaches to s...
It is well known that the use of aerodynamic forces to assist in orbital transfer can significantly ...
Abstract. Necessary conditions for minimax problems with isolated or flat maxima re presented. Some ...
Research results are presented of an investigation of the optimum maneuvers of advanced shuttle type...
[[abstract]]This paper presents the exact dimensionless equations of motion and the necessary condit...
Necessary conditions for minimax problems with isolated or flat maxima are presented. Some relevant ...
With the advent of aeroassist technology for orbital transfers, it is of interest to have explicit o...
A major problem with operations of lifting reentry vehicle having an aft center-of-gravity location ...
The aero-gravity assist maneuver is here proposed as a tool to improve the efficiency of the gravity...
This paper presents the optimal solu-tions to the maximum endurance subsonic by the application of P...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76170/1/AIAA-8575-707.pd
This paper considers the problem of optimizing the flight trajectory of a rocket vehicle moving in a...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76843/1/AIAA-1985-1817-421.pd
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
This paper presents the necessary conditions for solving Chebyshev minimax (or maximax) problems wit...
Control programs and flight paths of a hypersonic vehicle in climb are analyzed. Two approaches to s...
It is well known that the use of aerodynamic forces to assist in orbital transfer can significantly ...
Abstract. Necessary conditions for minimax problems with isolated or flat maxima re presented. Some ...
Research results are presented of an investigation of the optimum maneuvers of advanced shuttle type...
[[abstract]]This paper presents the exact dimensionless equations of motion and the necessary condit...