NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Dual Accelerometer Usage Strategy for Onboard Space NavigationThis work introduces a dual accelerometer usage strategy for onboard space navigation. In the proposed algorithm the accelerometer is used to propagate the state when its value exceeds a threshold and it is used to estimate its errors otherwise. Numerical examples and comparison to other accelerometer usage schemes are presented to validate the proposed approach.
Document ID
20120002557
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Zanetti, Renato (Draper (Charles Stark) Lab., Inc. Houston, TX, United States)
D'Souza, Chris (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 29, 2012
Subject Category
Astrodynamics
Report/Patent Number
JSC-CN-25550
AAS 12-198
Report Number: JSC-CN-25550
Report Number: AAS 12-198
Meeting Information
Meeting: 22nd AAS/AIAA Space Flight Mechanics Meeting
Location: Charleston, SC
Country: United States
Start Date: January 29, 2012
End Date: February 2, 2012
Sponsors: American Astronomical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available