Kalman filtering and smoothing and maximum likelihood estimation techniques were applied to the problem of estimating the aircraft state in nonsteady flight from onboard noisy inertial and barometric measurements. Applied to actual flight test data, the estimation schemes yielded similar results. (Author)
Estimation of the Aircraft State in Non-Steady Flight
1974
22 pages
Report
No indication
English
Steady aircraft flight and performance
TIBKAT | 2011
|Steady aircraft flight and performance
SLUB | 2011
|BOOK REVIEW - Steady Aircraft Flight and Performance
Online Contents | 2012
|Propulsive Efficiency and Aircraft Drag Determined From Steady State Flight Test Data
SAE Technical Papers | 1985
|