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== | ==Attitude Estimation and Control== | ||
* [[GPS_Attitude_Determination|GPS Attitude Determination]] | * [[GPS_Attitude_Determination|GPS Attitude Determination]] | ||
* [[ | * [[ISS_Leak_Localization from_Attitude_Response|ISS Leak Localization from Attitude Response]] | ||
* [[Robust_Spacecraft_Attitude_Determination_and_Control|Robust Spacecraft Attitude Determination and Control]] | * [[Robust_Spacecraft_Attitude_Determination_and_Control|Robust Spacecraft Attitude Determination and Control]] | ||
* [[Spacecraft_Formation_Flying_Navigation|Spacecraft Formation Flying Navigation]] | * [[Spacecraft_Formation_Flying_Navigation|Spacecraft Formation Flying Navigation]] | ||
* [[ | |||
==Data Fusion and General Estimation== | |||
* [[Geometric Integration|Geometric Integration]] | |||
* [[Generalized_Multiple-Model_Adaptive_Estimation|Generalized Multiple-Model Adaptive Estimation]] | |||
* [[Covariance Intersection|Covariance Intersection]] | |||
* [[Adaptive_Control_Using_Model_Error_Control_Synthesis|Adaptive Control Using Model-Error Control Synthesis]] | |||
==Navigation== | |||
* [[Solution_Method_for_Kepler's_Equation|Solution Method for Kepler's Equation]] | |||
==Space Situational Awareness== | |||
* [[Attribute_Estimation|Attribute Estimation]] | |||
==Center for Multisource Information Fusion== | |||
* [http://www.infofusion.buffalo.edu/ Center for Multisource Information Fusion] | |||
==Undergraduate Project Teams== | |||
* [http://nanosat.eng.buffalo.edu/ UB Nanosatellite Mission for Space Situational Awareness Club] | |||
* [http://www.ubseds.org/ UB SEDS CLub] | |||
* [http://www.ubaiaa.org/Home UB AIAA Club] |
Latest revision as of 22:24, 7 December 2015
Attitude Estimation and Control
- GPS Attitude Determination
- ISS Leak Localization from Attitude Response
- Robust Spacecraft Attitude Determination and Control
- Spacecraft Formation Flying Navigation
Data Fusion and General Estimation
- Geometric Integration
- Generalized Multiple-Model Adaptive Estimation
- Covariance Intersection
- Adaptive Control Using Model-Error Control Synthesis