Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973.Vita.Includes bibliographical references.Ph.D
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.In...
Cover title."May 1968."Includes bibliographical references (p. 24).Mode of access: Internet
Optimal multi-impulse trajectories were investigated as a nominal about which asymptotic expansion w...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mathematics, 1952.Vita.Includes bib...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.MIC...
Optimum three-impulse transfer from circular Earth parking orbit onto asymptotic velocity vector cha...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1960.In...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1982.MICROFI...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973.In...
textSpacecraft trajectory optimization is a topic of crucial importance to space missions design. Th...
The restricted three-body problem represents the dynamical framework employed for spacecraft mission...
Prepared at Lewis Research Center."March 1969"--Cover.Includes bibliographical references (p. 38).Mo...
Ph.D.Aerospace materialsEnergyUniversity of Michigan, Horace H. Rackham School of Graduate Studiesht...
A collection of typical three-body trajectories from the L1 libration point on the sun-earth line to...
Copyright © 2015 by the authors. Published by the American Institute of Aeronautics and Astronautics...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.In...
Cover title."May 1968."Includes bibliographical references (p. 24).Mode of access: Internet
Optimal multi-impulse trajectories were investigated as a nominal about which asymptotic expansion w...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mathematics, 1952.Vita.Includes bib...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.MIC...
Optimum three-impulse transfer from circular Earth parking orbit onto asymptotic velocity vector cha...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1960.In...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1982.MICROFI...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1973.In...
textSpacecraft trajectory optimization is a topic of crucial importance to space missions design. Th...
The restricted three-body problem represents the dynamical framework employed for spacecraft mission...
Prepared at Lewis Research Center."March 1969"--Cover.Includes bibliographical references (p. 38).Mo...
Ph.D.Aerospace materialsEnergyUniversity of Michigan, Horace H. Rackham School of Graduate Studiesht...
A collection of typical three-body trajectories from the L1 libration point on the sun-earth line to...
Copyright © 2015 by the authors. Published by the American Institute of Aeronautics and Astronautics...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.In...
Cover title."May 1968."Includes bibliographical references (p. 24).Mode of access: Internet
Optimal multi-impulse trajectories were investigated as a nominal about which asymptotic expansion w...
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