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Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters
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Application of a Constant Gain Extended Kalman Filter for in-flight estimation of aircraft engine performance parameters
ID:
3534398
Creatori:
(1389758) Simon, Donald L.
...
(1398039) Litt, Jonathan S.
...
(1419547) Kobayashi Takahisa
...
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