NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Sequential Probability Ratio Test for Collision Avoidance Maneuver Decisions Based on a Bank of Norm-Inequality-Constrained Epoch-State FiltersSequential probability ratio tests explicitly allow decision makers to incorporate false alarm and missed detection risks, and are potentially less sensitive to modeling errors than a procedure that relies solely on a probability of collision threshold. Recent work on constrained Kalman filtering has suggested an approach to formulating such a test for collision avoidance maneuver decisions: a filter bank with two norm-inequality-constrained epoch-state extended Kalman filters. One filter models 1he null hypothesis 1ha1 the miss distance is inside the combined hard body radius at the predicted time of closest approach, and one filter models the alternative hypothesis. The epoch-state filter developed for this method explicitly accounts for any process noise present in the system. The method appears to work well using a realistic example based on an upcoming highly-elliptical orbit formation flying mission.
Document ID
20180001183
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Carpenter, J. R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Markley, F. L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Alfriend, K. T.
(Texas A&M System Univ. College Station, TX, United States)
Wright, C.
(a.i. solutions, Inc. Lanham, MD, United States)
Arcido, J.
(a.i. solutions, Inc. Lanham, MD, United States)
Date Acquired
February 13, 2018
Publication Date
July 31, 2011
Subject Category
Astrodynamics
Report/Patent Number
AAS 11-437
LEGNEW-OLDGSFC-GSFC-LN-1150
Report Number: AAS 11-437
Report Number: LEGNEW-OLDGSFC-GSFC-LN-1150
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Girdwood, AK
Country: United States
Start Date: July 31, 2011
End Date: August 4, 2011
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available