Trajectory optimization of aerial slung load release for piloted helicopters-Reference-Cited by-同舟云学术

Trajectory optimization of aerial slung load release for piloted helicopters

Published:2021-02 Issue:2 Volume:34 Page:229-239
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

WANG Luofeng^ORCID,CHEN Renliang,YAN Xufei

Funder

Priority Academic Program Development of Jiangsu Higher Education Institutions

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference23 articles.

1. Epidemiology and prevention of helicopter external load accidents;Manwaring;J Safety Res,1998

2. Development of an efficient contact-friction model for high-fidelity cargo airdrop simulation;Ning;Chinese J Aeronaut,2019

3. Ronen T, Bryson AE, Jr, Hindson WS. Dynamics of a helicopter with a sling load. AIAA 13th atmospheric flight mechanics conference. Reston: AIAA; 1986.

4. Cicolani LS, Kanning G. Equations of motion of slung-load systems, including multilift systems. Washington, D.C.: NASA; 1992. Report No.: NASA-TP-3280.

5. Simulation of coupled helicopter–slung load–pilot dynamics;Enciu;J Am Helicopter Soc,2017

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