Published: 1975
Total Pages: 438
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Twenty-nine papers and comments are contained in these Proceedings. Several discuss and compare results obtained with different parameter identification techniques applied to specific fighter aircraft at high angles of attack, subsonic and supersonic transports, VTOL and STOL aircraft, and helicopters. Special problem areas such as systems modelling with high internally-generated fluctuations, aircraft state estimation in non-steady flight and parameter identification for non-linear aerodynamic regimes are covered. The sessions at the Specialists' Meeting were titled mathematical models, instrumentation and filters, flight test techniques, analysis of flight test data, rotorcraft parameter identification and selected topics.
