Global ETD Search
Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.
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Showing 1 to 4 of 4 for “"Thrust acceleration"”.
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Nonlinear feedback solution for minimum-time intercept with constant thrust acceleration.
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.
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Applications of Second-Order Necessary and Sufficient Conditions to Optimal Trajectories
… spacecraft trajectory problems with constant thrust acceleration and with time-varying low thrust acceleration for a power-limited rocket engine. A solution that simultaneously maximizes final orbit energy and minimizes propellant consumption is found that satisfies the usual first-order …
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Spacecraft trajectory optimization using many embedded Lambert problems
… short arcs simultaneously approximate low thrust and eliminates the need to know the structure of a high-thrust impulsive-maneuver solution. A set of examples show the EBVP technique to be efficient, robust, and useful. In particular, an example using 256 revolutions, 6143 segments, and a …
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In-Flight control simulation of a proposed, future microsatellite for the African Resource Management Constellation (ARMC)
… raise manoeuvre was not successful due to the thrust acceleration not overcoming atmospheric drag. The simulation of the Gecko camera and the electric propulsion system into the SimTG was successful. All objectives were completed, and the enhancement of the flight software was successful and …