Status of Dynamic Flight Test Technology -Model Identification for Flight Simulation Delft Univ. of Technology

Format:

Conference/Event

Author/Creator:

Mulder, J. A., author.

Conference Name:

Business Aircraft Meeting and Exposition (1981-04-07 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1981

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

810597

Access Restriction:

Restricted for use by site license