Model Based Parameter Estimation for a Missile
Traditionally direct integration of the measurements from an IMU (inertial measuring unit), measuring the acceleration and inertial angular velocity of the missile, is used to determine a missiles position and state. However, if some prior information about the missile dynamics is known, this method...
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| Format: | Others |
| Language: | English |
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KTH, Reglerteknik
2009
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-105713 |