TY - GEN
T1 - Development of fault tolerant integrated INS/RADAR altimeter using adaptive filtration algorithm with the filter gain correction
AU - Hajiyev, Ch
PY - 2006
Y1 - 2006
N2 - Radar Altimeter, Kalman Filter The fault tolerant integrated navigation system, consisting of radar and inertial altimeters, is presented. The integration is achieved by using an adaptive Kalman filter with the filter gain correction. In the open loop system, the inertial altimeter is the main source of information, and radar altimeter provides discrete aiding data to support the estimations. The performance of the proposed fault tolerant integrated radar/inertial altimeter in case of abrupt faults is examined.
AB - Radar Altimeter, Kalman Filter The fault tolerant integrated navigation system, consisting of radar and inertial altimeters, is presented. The integration is achieved by using an adaptive Kalman filter with the filter gain correction. In the open loop system, the inertial altimeter is the main source of information, and radar altimeter provides discrete aiding data to support the estimations. The performance of the proposed fault tolerant integrated radar/inertial altimeter in case of abrupt faults is examined.
KW - Inertial navigation
KW - Integrated navigation systems
UR - https://www.scopus.com/pages/publications/84913591616
M3 - Conference contribution
AN - SCOPUS:84913591616
T3 - 13th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2006 - Proceedings
SP - 175
EP - 177
BT - 13th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2006 - Proceedings
A2 - Peshekhonov, Vladimir G.
A2 - Afanasova, I.S.
PB - State Research Center of the Russian Federation
T2 - 13th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2006
Y2 - 29 May 2006 through 31 May 2006
ER -