NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Current-State Constrained Filter Bank for Wald Testing of Spacecraft ConjunctionsWe propose a filter bank consisting of an ordinary current-state extended Kalman filter, and two similar but constrained filters: one is constrained by a null hypothesis that the miss distance between two conjuncting spacecraft is inside their combined hard body radius at the predicted time of closest approach, and one is constrained by an alternative complementary hypothesis. The unconstrained filter is the basis of an initial screening for close approaches of interest. Once the initial screening detects a possibly risky conjunction, the unconstrained filter also governs measurement editing for all three filters, and predicts the time of closest approach. The constrained filters operate only when conjunctions of interest occur. The computed likelihoods of the innovations of the two constrained filters form a ratio for a Wald sequential probability ratio test. The Wald test guides risk mitigation maneuver decisions based on explicit false alarm and missed detection criteria. Since only current-state Kalman filtering is required to compute the innovations for the likelihood ratio, the present approach does not require the mapping of probability density forward to the time of closest approach. Instead, the hard-body constraint manifold is mapped to the filter update time by applying a sigma-point transformation to a projection function. Although many projectors are available, we choose one based on Lambert-style differential correction of the current-state velocity. We have tested our method using a scenario based on the Magnetospheric Multi-Scale mission, scheduled for launch in late 2014. This mission involves formation flight in highly elliptical orbits of four spinning spacecraft equipped with antennas extending 120 meters tip-to-tip. Eccentricities range from 0.82 to 0.91, and close approaches generally occur in the vicinity of perigee, where rapid changes in geometry may occur. Testing the method using two 12,000-case Monte Carlo simulations, we found the method achieved a missed detection rate of 0.1%, and a false alarm rate of 2%.
Document ID
20120016758
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Carpenter, J. Russell
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Markley, F. Landis
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 26, 2013
Publication Date
October 29, 2012
Subject Category
Astrodynamics
Report/Patent Number
GSFC.CP.7474.2012
Report Number: GSFC.CP.7474.2012
Meeting Information
Meeting: 23rd International Symposium on Space Flight Dynamics
Location: Pasadena, CA
Country: United States
Start Date: October 29, 2012
End Date: November 2, 2012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available