The accuracy of aircraft stability and control derivatives as estimated from dynamic response measurements depends on the form of the time histories of the control inputs. After selecting a suitable criterion and imposing constraints on either the aircraft's state or the control inputs it is possible to optimize the form of these time histories. A method for control input optimization is proposed which avoids some disadvantages of earlier methods and was successfully applied in the design of longitudinal and lateral flight test maneuvers.
Optimal Inputs for Aircraft Parameter Estimation
1989
36 pages
Report
Keine Angabe
Englisch
Optimal input design for aircraft parameter estimation
Elsevier | 2005
|AIAA | 1987
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