Flight Dynamic Characteristics of Tiltrotor Aircraft Slung-Load System-Reference-Cited by-同舟云学术

Flight Dynamic Characteristics of Tiltrotor Aircraft Slung-Load System

Published:2017-05 Issue:3 Volume:54 Page:1221-1228
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Cao Yihua¹,Qi Qi¹,Zhang Dongfang¹

Affiliation:

1. Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033937

Reference13 articles.

1. MaiselM. D.GiulianettiD. J.DuganD. C. “The History of the XV-15 Tilt-Rotor Aircraft: From Concept to Flight,” NASA Rept. SP-2000-4517, Washington, D. C. 2000.

2. RosensteinH.McVeighM. A.MollenkofP. A. “V/STOL Tilt-Rotor Aircraft Study Mathematical Model for a Real Time Simulation of a Tilt-Rotor Aircraft (Boeing Model 222),” NASA Rept. CR-114601, April 1973.

3. FergusonS. W. “A Mathematical Model for Real Time Flight Simulation of a Generic Tilt-Rotor Aircraft,” NASA Rept. CR-166536, 1988.

4. KleinhesselinkK. M. “Stability and Control Modeling of Tilt-Rotor Aircraft,” M.S. Thesis, Univ. of Maryland, College Park, MD, 2007.

5. CicolaniL. S.KanningG. “Equations of Motion of Slung-Load Systems with the Results for Dual Lift,” NASA Rept. TM-102246, Feb. 1990.

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