Add to ORKGThesis. 1978. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS.Vita.Includes bibliographical references.Ph.D
The optimal control of orbital transfers is considered (problem proposed by the French Space Agency)...
AbstractLow-thrust Earth-orbit transfers with 10−5-order thrust-to-weight ratios involve a large num...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1960.In...
The problem of minimum-time, constant-thrust orbital transfer between coplanar circular orbits is re...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.In...
It is well known that the use of aerodynamic forces to assist in orbital transfer can significantly ...
In view of the increasing human activity in space, the maneuvering between different orbits is going...
This thesis considers both classical and minimax problems of optimal control arising in the study of...
Title from PDF of title page (University of Missouri--Columbia, viewed on July 29, 2013).The entire ...
textSpacecraft trajectory optimization is a topic of crucial importance to space missions design. Th...
In the present paper several strategies for impulsive orbit transfer between circular orbits are com...
Minimum-fuel orbital transfer between elliptical orbits is studied by first analyzing separately the...
The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of consta...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1965. Sc.D.Bib...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
The optimal control of orbital transfers is considered (problem proposed by the French Space Agency)...
AbstractLow-thrust Earth-orbit transfers with 10−5-order thrust-to-weight ratios involve a large num...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1960.In...
The problem of minimum-time, constant-thrust orbital transfer between coplanar circular orbits is re...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.In...
It is well known that the use of aerodynamic forces to assist in orbital transfer can significantly ...
In view of the increasing human activity in space, the maneuvering between different orbits is going...
This thesis considers both classical and minimax problems of optimal control arising in the study of...
Title from PDF of title page (University of Missouri--Columbia, viewed on July 29, 2013).The entire ...
textSpacecraft trajectory optimization is a topic of crucial importance to space missions design. Th...
In the present paper several strategies for impulsive orbit transfer between circular orbits are com...
Minimum-fuel orbital transfer between elliptical orbits is studied by first analyzing separately the...
The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of consta...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1965. Sc.D.Bib...
This thesis discusses optimal trajectories for hypervelocity flight of interest in aeroassisted orbi...
The optimal control of orbital transfers is considered (problem proposed by the French Space Agency)...
AbstractLow-thrust Earth-orbit transfers with 10−5-order thrust-to-weight ratios involve a large num...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1960.In...