Direct Methodology for Constrained System Analysis with Applications to Aircraft Dynamics-Reference-Cited by-同舟云学术

Direct Methodology for Constrained System Analysis with Applications to Aircraft Dynamics

Published:2017-11 Issue:6 Volume:54 Page:2378-2385
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Vora Anuj S.¹,Sinha Nandan K.¹

Affiliation:

1. Indian Institute of Technology Madras, Chennai 600 036, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034264

Reference20 articles.

1. StrogatzS. H., Nonlinear Dynamics and Chaos, Westview, Cambridge, MA, 1994, pp. 150–151.

2. CummingsP. A. “Continuation Methods for Qualitative Analysis of Aircraft Dynamics,” NASA CR-2004-213035, 2014.

3. Level Flight Trim and Stability Analysis Using Extended Bifurcation and Continuation Procedure

4. SinhaN. K.AnanthkrishnanN., Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods, CRC Press, Boca Raton, FL, Oct. 2013, pp. 319–320.

5. DoedelE. J.ChampneysA. R.FairgrieveT.KuznetsovY. A.OldemanB. E.PaffenrothR.SandstedeB.WangX.ZhangC. “AUTO-07P: Continuation and Bifurcation Software for Ordinary Differential Equations,” Technical Rept. Concordia Univ., Montreal, Canada, 2008.

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