Extension of the Neal-Smith criteria-based H-infinity-modeling technique to LAHOS data
Author:
Affiliation:
1. Kyushu Univ., Fukuoka, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4251
Reference50 articles.
1. Neal,T.P. and Smith,R.E. "An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes,"Flight Dynamics Lab.,Wright-Patterson AFB.,OH., AFFDL-TR-70-74, Vols.I and I, Dec. 1970.
2. Chalk,C.R., Difranco,D.A., Lebacqz,J.V. and Neal,T.R, "Revisions to MIL-F-8785B (ASG) Proposed by Cornell Aeronautical Laboratory under Contract F33615-71-cl 254,"Flight Dynamics Lab.,Wright-Patterson AFB.,OH., AFFDL-TR-72-41,Apr. 1972.
3. Ashkenas,I.L., Hoh,R.H. and Craig,S.J. "Recommended Revisionsto Selected Portions of MIL-F-8785B(ASG) and Background Data,"FlightDynamicsLab.,Wright-Patterson AFB.,OH., AFFDL-TR-73-76, Aug. 1973.
4. An improved approach to predicting pilot rating behavior
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