Status of Dynamic Flight Test Technology -Model Identification for Flight Simulation 810597
Dynamic flight test technology has by now emerged as a valuable tool for assessment of aircraft performance characteristics and stability and control characteristics. In this paper emphasis is on applications In the context of flight simulation. It is shown that after flight path reconstruction and reconstruction of the motion of the primary control system a linear and stepwise identification procedure can be applied for the development of aerodynamic models and models of primary control force characteristics. These models can be implemented in mathematical models for aircraft flight simulation.
Citation: Mulder, J. and den Hollander, J., "Status of Dynamic Flight Test Technology -Model Identification for Flight Simulation," SAE Technical Paper 810597, 1981, https://doi.org/10.4271/810597. Download Citation
Author(s):
J. A. Mulder, J. G. den Hollander
Affiliated:
Delft Univ. of Technology
Pages: 19
Event:
Business Aircraft Meeting and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 1981Transactions-V90-A
Related Topics:
Simulators
Mathematical models
Flight tests
Control systems
Aircraft
Aerodynamics
Identification
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