Analysis and order reduction of an autonomous lunar lander navigation system
A navigation system for precision lunar descent and landing is presented and analyzed. The navigation algorithm is based upon the extended Kalman Filter and employs measurements from an inertial measurement unit to propagate the vehicle position, velocity, and attitude forward in time. External meas...
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| Format: | Others |
| Language: | English |
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2012
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| Online Access: | http://hdl.handle.net/2152/ETD-UT-2009-08-359 |