Application of Improved Extended Kalman Filter for Adaptive Model of Aircraft Engine
2014 ◽
Vol 709
◽
pp. 180-185
Keyword(s):
Adaptive model is the basis of engine fault diagnosis, performance monitoring, engine control, etc. This paper presents an improved kalman filter method which uses engine measurable parameters deviation to estimate the degradation parameters to correct the nominal model, and the acquisition and application of multiple kalman filter gain matrices in the whole flight envelope is analyzed. Simulation is carried out taking a civil engine as simulation object, the simulation results show that the method used in this paper to establish unmeasured parameters adaptive model can get the engine parameters better.
Keyword(s):
2014 ◽
Vol 262
◽
pp. 50-61
◽
Keyword(s):
A two-stage extended kalman filter method for fault estimation of satellite attitude control systems
2017 ◽
Vol 354
(2)
◽
pp. 872-886
◽
Keyword(s):
2018 ◽
Vol 2018
◽
pp. 1-10
◽
Keyword(s):
2021 ◽
Vol 9
(VII)
◽
pp. 3083-3089
Keyword(s):
2014 ◽
Vol 701-702
◽
pp. 449-452