NDLI: Kalman filter for mass property and thrust identification (mms)

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Kalman filter for mass property and thrust identification (mms)

Content Provider	NASA Technical Reports Server (NTRS)
Author	Queen, Steven
Copyright Year	2015
Description	The Magnetospheric Multiscale (MMS) mission consists of four identically instrumented, spin-stabilized observatories, elliptically orbiting the Earth in a tetrahedron formation. For the operational success of the mission, on-board systems must be able to deliver high-precision orbital adjustment maneuvers. On MMS, this is accomplished using feedback from on-board star sensors in tandem with accelerometers whose measurements are dynamically corrected for errors associated with a spinning platform. In order to determine the required corrections to the measured acceleration, precise estimates of attitude, rate, and mass-properties is necessary. To this end, both an on-board and ground-based Multiplicative Extended Kalman Filter (MEKF) were formulated and implemented in order to estimate the dynamic and quasi-static properties of the spacecraft.
File Size	42191855
Page Count	26
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20150023412
Archival Resource Key	ark:/13960/t3kx0dh6s
Language	English
Publisher Date	2015-10-20
Access Restriction	Open
Subject Keyword	Maneuver and Attitude Dynamics Determination and Control Format Flying Accelerometers Dynamic Characteristics Calibrating Airborne/spaceborne Computers Nasa Space Programs Ground Stations Errors Attitude Inclination Magnetic Field Reconnection Center of Mass Star Trackers Thrust Vector Control Navigation Aids Inertia Kalman Filters State Estimation Orbital Maneuvers Thrust Navigation Instruments Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Presentation

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