Research: Difference between revisions
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* Geometric Integration | * Geometric Integration | ||
* Kepler's Problem | * Kepler's Problem | ||
* Nanosatellite Mission for Space Situational Awareness | * [http://nanosat.eng.buffalo.edu/ Nanosatellite Mission for Space Situational Awareness] | ||
* [[Adaptive_Control_Using_Model_Error_Control_Synthesis|Adaptive Control Using Model-Error Control Synthesis]] | * [[Adaptive_Control_Using_Model_Error_Control_Synthesis|Adaptive Control Using Model-Error Control Synthesis]] | ||
* [[GPS_Attitude_Determination|GPS Attitude Determination]] | * [[GPS_Attitude_Determination|GPS Attitude Determination]] |
Revision as of 04:25, 13 March 2012
- Space Situational Awareness
- High Fidelity Orbit Simulation
- Spacecraft Attitude Sensors and Actuator Calibration
- Data Fusion
- Estimation Theory
- Attitude Determination using Laser Communication Devices
- Geometric Integration
- Kepler's Problem
- Nanosatellite Mission for Space Situational Awareness
- Adaptive Control Using Model-Error Control Synthesis
- GPS Attitude Determination
- CEGANS Sensor
- Robust Spacecraft Attitude Determination and Control
- Spacecraft Formation Flying Navigation
- Space Station Leak Localization from Attitude Response