Study on the chaotic dynamics in yaw–pitch–roll coupling of asymmetric rolling projectiles with nonlinear aerodynamics-Reference-Cited by-同舟云学术

Study on the chaotic dynamics in yaw–pitch–roll coupling of asymmetric rolling projectiles with nonlinear aerodynamics

Published:2019-08-05 Issue:4 Volume:97 Page:2739-2756
ISSN:0924-090X
Container-title:Nonlinear Dynamics
language:en
Short-container-title:Nonlinear Dyn

Author:

Xu Yanli,Yue Baozeng^ORCID,Yang Zhengmao,Zhao Liangyu,Yang Shuxing

Funder

National Natural Science Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s11071-019-05159-3.pdf

Reference47 articles.

1. Nicolaides, J.D.: On the free flight motion of missiles having slight configurational asymmetries. U. S. Army Ballistic Research Lab, Aberdeen Proving Ground, MD, BRL Rept. 858, 1952, AD 26405

2. also, Institute of Aeronautical Sciences Paper 395 (1952)

3. Nicolaides, J.D.: Two nonlinear problems in the flight dynamics of modern ballistic missiles. Report 59-17, Institute of the Aeronautical Sciences (1959)

4. Price Jr., D.A.: Sources, mechanisms and control of roll resonance phenomena for sounding rockets. J. Spacecr. Rockets 4, 1516–1525 (1967)

5. Murphy, C.H.: Some special cases of spin-yaw lock-in. J. Guidance Control Dyn. 12, 771–776 (1989)

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