Add to ORKGPeer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77164/1/AIAA-1972-931-894.pd
With the advent of aeroassist technology for orbital transfers, it is of interest to have explicit o...
In previous research, an aircraft trajectory planning algorithm was developed aiming at optimizing ...
Research is summarized on optimal trajectories for the aeroassisted flight experiment, performed by ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Approximate solutions for flight path angle of reentry vehicle in upper atmospher
The determination of optimal trajectories for the aero-assisted flight experiment (AFE) is investiga...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007.In...
The aeroassisted flight experiment (AFE) is to simulate a transfer from a geosynchronous Earth orbit...
A mathematical model, employing a modification of Chapman's nondimensional variables, is used to des...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76344/1/AIAA-1993-3679-680.pd
The general solution for the optimum three-dimensional aerodynamic control of a lifting vehicle ente...
The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...
Note:Planetary gravity assist is used to increase or decrease the heliocentric velocity of the space...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77164/1/AIAA-1972-931-894.pd
With the advent of aeroassist technology for orbital transfers, it is of interest to have explicit o...
In previous research, an aircraft trajectory planning algorithm was developed aiming at optimizing ...
Research is summarized on optimal trajectories for the aeroassisted flight experiment, performed by ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Approximate solutions for flight path angle of reentry vehicle in upper atmospher
The determination of optimal trajectories for the aero-assisted flight experiment (AFE) is investiga...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2007.In...
The aeroassisted flight experiment (AFE) is to simulate a transfer from a geosynchronous Earth orbit...
A mathematical model, employing a modification of Chapman's nondimensional variables, is used to des...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76344/1/AIAA-1993-3679-680.pd
The general solution for the optimum three-dimensional aerodynamic control of a lifting vehicle ente...
The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...
Note:Planetary gravity assist is used to increase or decrease the heliocentric velocity of the space...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77164/1/AIAA-1972-931-894.pd
With the advent of aeroassist technology for orbital transfers, it is of interest to have explicit o...
In previous research, an aircraft trajectory planning algorithm was developed aiming at optimizing ...