Verification & validation of a UH-60 FLIGHTLAB® model in support of the UH-60M limited user test

Annual Forum Proceedings - American Helicopter Society

Volumn 2, Issue , 2004, Pages 1267-1275

  Strope, Kris ^a   Borden, Christopher ^a   Harding, Jeff ^b  

^a Aviation Engineering Directorate   (United States)

^b Harding Consulting Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COCKPIT INSTRUMENTS; COCKPIT TEST BED (CTB); CONTROL LINKAGES; FLIGHT HARDWARE;

ACTUATORS; COCKPITS (AIRCRAFT); CORRELATION METHODS; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; FLIGHT SIMULATORS; MATHEMATICAL MODELS;

AEROSPACE ENGINEERING;

EID: 4143124387     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Nikonchuk, Will, "Verification and Validation Plan for the Models and Simulations and Equipment Used in the UH-60M cockpit test bed of the UH-60 System Integration Laboratory", SED-BMCTB-WP-0001, August 2003.
2. FAA Advisory Circular 120-63," Helicopter Simulator Qualification", AC120-63, October 1994.
3. Cicolani, Luigi, et al, "Flight-Time Identification of a UH-60A Helicopter and Slung Load," NATO RTO SCI Panel Symposium, RTO-MP-11, Madrid, Spain, May 1998.
4. Williams, J.N., Ham, J.A., and Tishler, M.B., "Flight Test Manual: Rotorcraft Frequency Domain Flight Testing," U.S. Army Aviation Technical Test Center, Airworthiness Qualification Test Directorate, Project No. 93-14, September 1995.
5. Tischler, M.B., and Cauffman, M.G., "Frequency-Response Method for Rotorcraft System Identification: Flight Application to BO-105 Coupled Rotor/Fuselage Dynamics," Journal of the American Helicopter Society, vol. 37, no. 3, Jul 1992, pp.3-17.
6. Hoh, R.H., et al, "Proposed MIL Standard and Handbook - Flying Qualities of Air Vehicles", AFWAL-TR-82-3081 Vol II, Nov 1982.
7. Tischler, M.B., "System Identification Methods for Aircraft Flight Control Development and Validation," Published in Advances in Aircraft Flight Control, Taylor & Francis, 1996.
8. Fletcher, J.W., "Identification of UH-60 Stability Derivative Models in Hover from Flight Test Data," American Helicopter Society Annual Forum, St. Louis, Missouri, May 1993.
9. He, C., Lee, C.S., and Chen, W., "Rotorcraft Simulation Model Enhancements to Support Design, Testing and Operational Analysis," Journal of the American Helicopter Society, Vol. 45, October 2000.
10. Mansur, M.H., and Tischler, M.B., "An Empirical Correction for Improving Off-Axes Response in Flight Mechanics Helicopter Models," AGARD Flight Vehicle Integration Panel Symposium on "Advances in Rotorcraft Technology," Ottawa, Canada, May 1996.
11. Aeronautical Design Standard, Performance Specification, "Handling Qualities Requirements for Military Rotorcraft," U.S. Army Aviation Missile Command, Aviation Engineering Directorate, ADS-33E-PRF, March 2000.