Computer Simulation of a Rotational Single-Element Flexible Spacecraft Boom.
NAVAL POSTGRADUATE SCHOOL MONTEREY CA
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The requirement to develop a space based remote ocean sensing platform exists within the Department of the Navy. This project models a satellite subsystem with structural flexibility utilizing the Equivalent Rigid Link System ERLS. Dynamic analysis with computer simulation is presented for a simple flexible boom rotating in three dimensions with and without a point mass at the boom tip. Keywords Theses Flexible manipulators Equations of motion. Author
- Unmanned Spacecraft
- Computer Programming and Software
- Physical and Dynamic Oceanography