Dynamic Coupling of the KC-135 Tanker and Boom for Modeling and Simulation-Reference-Cited by-同舟云学术

Dynamic Coupling of the KC-135 Tanker and Boom for Modeling and Simulation

Published:2007-05 Issue:3 Volume:44 Page:1034-1039
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Smith Austin L.¹,Kunz Donald L.²

Affiliation:

1. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio, 45433

2. U.S. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio, 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.27241

Reference6 articles.

1. Campbell, T. G., Durkkley, G. D., Fletcher, J. J., Hutchings, S. J., Lee, J. H., Manley, T. J., Przybysz, J., and Roberts, R. W. "System Study of the KC-135 Aerial Refueling System, Vols. 1 and 2," M.S. Thesis, Department of Aeronautics and Astronautics,U.S. Air Force Institute of Technology, Wright-Patterson AFB, OH,1989.

2. The Structure of Multibody Dynamics Equations

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Super-Twisting Sliding Mode Controller Based on Extended State Observer of Flying Boom;2023 China Automation Congress (CAC);2023-11-17

2. ESO-based nonlinear flying boom attitude control with the handling qualities requirement;Aerospace Science and Technology;2022-01

3. Adaptive Backstepping Fast Terminal Sliding Mode Controller for Refueling Boom with Elastic;Lecture Notes in Electrical Engineering;2021-10-30

4. Cooperative Docking Guidance and Control with Application to Civil Autonomous Aerial Refueling;Journal of Guidance, Control, and Dynamics;2021-09

5. Adaptive Fast Terminal Sliding Mode Control for Automatic Load Alleviation Problem of Refueling Boom Against Disturbances;2021 33rd Chinese Control and Decision Conference (CCDC);2021-05-22