Performance Metrics for Tiltrotor Flight Dynamics During the Transition Regime-Reference-Cited by-同舟云学术

Performance Metrics for Tiltrotor Flight Dynamics During the Transition Regime

Published:2014-11 Issue:6 Volume:37 Page:2039-2044
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Sunkara Vishwamithra¹,Nobleheart Wilfred¹,Chakravarthy Animesh¹

Affiliation:

1. Department of Electrical Engineering, Wichita State University, Wichita, Kansas 67260

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000310

Reference17 articles.

1. “Military Specification: Flying Qualities of Piloted Airplanes,” U.S. Dept. of Defense MIL-SPEC MIL-F-8785C, Nov. 1980.

2. “General Specification for Flight Control Systems Design, Installation and Test of Piloted Aircraft,” U.S. Dept. of Defense MIL-SPEC MIL-DTL-9490E, April 2008.

3. “Military Specification Flying Qualities for V/STOL Aircraft,” U.S. Dept. of Defense MIL-SPEC MIL-F-83300, Nov. 1970.

4. “Aeronautical Design Standard Performance Specification Handling Qualities Requirements for Military Rotorcraft,” U.S. Army Aviation and Missile Command Aeronautical Design Standard ADS-33-E-PRF, March 2000.

5. BlankenC. L.HohR. H.MitchellD. G.KeyD. L. “Test Guide for ADS-33-E-PRF,” HOH Aeronautics Rept. HAI-TR-1130-1, Lomita, CA, July 2008.

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