TY - JOUR
T1 - Mode estimation via conditionally linear filtering
T2 - Application to gyro failure monitoring
AU - Choukroun, Daniel
AU - Speyer, Jason L.
N1 - Funding Information:
This work was sponsored by the U.S. Air Force Office of Scientific research under grant F49620-01-1-0361 and by NASA Ames Research Center under grant NAG2-1484:4. This research was also supported by the Israel Science foundation under grant 1546/08.
PY - 2012/1/1
Y1 - 2012/1/1
N2 - This work introduces a novel approximate nonlinear filtering paradigm for nonlinear non-Gaussian discrete-time systems. Hinging on the concept of conditional orthogonality of random sequences, the conditionally linear filtering approach is an extension of the classical linear filtering approach. The resulting estimator turns out to be conditionally linear with respect to the most recent measurement, given the passed observations, which is adequate for online filtering. It is shown that the classical Kalman filter and the conditionally Gaussian filter, i.e., the optimal filter for conditionally linear Gaussian systems, are special cases of the conditionally linear filter. When applied to the problem of mode estimation in jump-parameter systems with full state information, it provides an approximate nonlinear mode estimator that only requires the first two moments of the process noise, whereas the optimal filter (Wonham filter) requires the complete noise distribution. In the case of noisy measurements in jump-linear systems, the conditionally linear filtering approach lends itself to a meaningful hybrid estimator. The proposed hybrid estimator is successfully applied to the problem of gyro failure monitoring onboard spacecraft using noisy attitude quaternion measurements. Extensive Monte Carlo simulations show that the conditionally linear mode estimator outperforms the linear mode estimator. For Gaussian noises the conditionally linear filter and the optimal Wonham filter perform similarly. Moreover, for Weibull-type noises, the conditionally linear filter outperforms a Wonham filter that assumes Gaussian noises.
AB - This work introduces a novel approximate nonlinear filtering paradigm for nonlinear non-Gaussian discrete-time systems. Hinging on the concept of conditional orthogonality of random sequences, the conditionally linear filtering approach is an extension of the classical linear filtering approach. The resulting estimator turns out to be conditionally linear with respect to the most recent measurement, given the passed observations, which is adequate for online filtering. It is shown that the classical Kalman filter and the conditionally Gaussian filter, i.e., the optimal filter for conditionally linear Gaussian systems, are special cases of the conditionally linear filter. When applied to the problem of mode estimation in jump-parameter systems with full state information, it provides an approximate nonlinear mode estimator that only requires the first two moments of the process noise, whereas the optimal filter (Wonham filter) requires the complete noise distribution. In the case of noisy measurements in jump-linear systems, the conditionally linear filtering approach lends itself to a meaningful hybrid estimator. The proposed hybrid estimator is successfully applied to the problem of gyro failure monitoring onboard spacecraft using noisy attitude quaternion measurements. Extensive Monte Carlo simulations show that the conditionally linear mode estimator outperforms the linear mode estimator. For Gaussian noises the conditionally linear filter and the optimal Wonham filter perform similarly. Moreover, for Weibull-type noises, the conditionally linear filter outperforms a Wonham filter that assumes Gaussian noises.
UR - http://www.scopus.com/inward/record.url?scp=84860366823&partnerID=8YFLogxK
U2 - 10.2514/1.48199
DO - 10.2514/1.48199
M3 - Article
AN - SCOPUS:84860366823
SN - 0731-5090
VL - 35
SP - 632
EP - 644
JO - Journal of Guidance, Control, and Dynamics
JF - Journal of Guidance, Control, and Dynamics
IS - 2
ER -