Optimal command generation for maneuvering the space station /
The objective of this research is to obtain near minimum-fuel and minimum-time maneuver commands for large-angle maneuvers for the international space station. Attitude and angular velocity waypoints are generated using the method of differential inclusion. This approach, motivated by the inverse...
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| Format: | Thesis eBook |
| Language: | English |
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[Place of publication not identified] :
[publisher not identified] ;
2001.
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| Online Access: | Link to OAKTrust copy |
Internet
Link to OAKTrust copyCushing: Theses & Dissertations Microforms (Does not check out)
| Call Number: |
2001 Thesis B79 |
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| Call Number | Status | Get It |
| 2001 Thesis B79 | Available | |
Available Online
| Call Number: |
2001 Thesis B79 |
|
|---|---|---|
| Call Number | Status | Get It |
| 2001 Thesis B79 | Available | |