Modelling Aircraft Dynamics
Abstract
A review has been made of the approaches currently under development for the modelling of aircraft flight dynamics at high angles-of-attack. The review is based on current research literature and on discussions held during an overseas visit carried out for the purpose of technical updating in the areas of flight dynamic modelling and parameter estimation. Keywords: Flight dynamics; High angle of attack; Mathematical models; Flight tests; Parameters; Data reduction; Australia.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1988
- Accession Number
- ADA204086
Entities
People
- C. A. Martin