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Optimal, low-thrust, earth-moon orbit transfer
Albert L. Herman,
Bruce A. Conway
Aerospace Engineering
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Keyphrases
Low-thrust
100%
Optimal Trajectory
100%
Orbit Transfer
100%
Earth-Moon
100%
Nonlinear Programming
50%
Collocation
50%
Transfer Time
50%
Flight Time
50%
Propellant
50%
Travel Time
50%
Vehicle Dynamics
50%
Propulsion System
50%
Specific Impulse
50%
Two-body Problem
50%
Acceleration Magnitude
50%
Earth Orbit
50%
Earth Gravity
50%
Lunar Orbit
50%
Engineering
Optimal Trajectory
100%
Thrust Acceleration
100%
Orbital Transfer
100%
Time-of-Flight
50%
Body Problem
50%
Vehicle Dynamics
50%
Propulsion System
50%
Specific Impulse
50%
Physics
The Moon
100%
Transfer Orbit
100%
Flight Time
50%
Spacecraft
50%
Earth Orbit
50%
Two Body Problem
50%
Lunar Orbit
50%
Earth Gravity
50%