An analysis of the time-domain neal-smith criterion

23rd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1998, Pages 154-162

  Foringer, Lori Ann ^a   Leggett, David B ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

RESEARCH LABORATORIES;

AIR FORCE RESEARCH LABORATORY; FLIGHT TEST; FLIGHT TEST DATA; PAPER DOCUMENTS; PILOT-INDUCED OSCILLATIONS; TIME DOMAIN NEAL SMITH CRITERIONS;

TIME DOMAIN ANALYSIS;

EID: 84983127756     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4250     Document Type: Conference Paper

References (9)

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2. Smith, Rogers E. Effects of Control System Dynamics on Fighter Approach and Longitudinal Flying Qualities. Technical Report AFFDL-TR-78-122, Wright-Patterson AFB, OH: Air Force Flight Dynamics Laboratory, March 1978.
3. Berthe, C. J., Chalk, C. R., and Sarrafian, S. Pitch Rate Flight Control Systems in the Flared Landing Task and Design Criteria Development. Technical Report NASA-CR-172491, October 1984.
4. Kish, Brian A., et al. A Limited Flight Test Investigation of Pilot-Induced Oscillation Due to Rate Limiting. AIAA-97-3703-CP, Atmospheric Flight Mechanics Conference, 11-13 August 1997.
5. Kish, Brian A Limited Flight Test Investigation of Pilot-Induced Oscillation Due to Rate Limiting (HAVE LIMITS). Technical Report AFFTC-TR-97-12, Edwards AFB, CA: Air Force Flight Test Center, August 1997.
6. Neal, T. P. and Rogers E. Smith. An InFlight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Technical Report AFFDL-TR-7074, Wright-Patterson AFB, OH: Air Force Flight Dynamics Laboratory, December 1970.
7. Onstott, E. D. and W. H. Faulkner Prediction, Evaluation and Specification of Closed Loop and Multiaxis Flying Qualities. Technical Report AFFDL-TR-78-3, Wright-Patterson AFB, OH: Air Force Flight Dynamics Laboratory, February 1978.
8. Crassidis, A. L. NT-33A Air Force Test Pilot School Spring '97 Test Management Projects Analysis and Results. Calspan SRL Corporation Document TM-056-NT33A-0674-ROO, Buffalo NY, September 1997.
9. Flying Qualities of Piloted Aircraft. Military Standard 1797A. Washington D. C.: Government Printing Office, 30 January 1990.