Cross-coupling between longitudinal and lateral aircraft dynamics ina spiral dive-Reference-Cited by-同舟云学术

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Cross-coupling between longitudinal and lateral aircraft dynamics ina spiral dive

Published:1983-01 Issue:1 Volume:20 Page:21-26
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Velger M.¹,Shinar J.¹

Affiliation:

1. Technion—Israel Institute of Technology, Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.44823

Reference19 articles.

1. 2Phillips, W.H. ^'Effect of Steady Rolling on Longitudinal and Directional Stability," NACA TN-1627, June 1948.

2. 3Sternfield, L. "A Simplified Method for Approximating the Transient Motion in Angles of Attack and Sideslip During a Constant Rolling Maneuver," NACA Report 1344, 1958.

3. A Theoretical and Experimental Study of Airplane Dynamics in Large-Disturbance Maneuvers

Cited by 1 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. Aircraft Spiral Recovery with Altitude Control;AIAA SCITECH 2022 Forum;2022-01-03

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