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Maximum steady roll rate in zero-sideslip roll maneuvers of aircraft

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This article is published in Journal of Aircraft.The article was published on 2002-09-01. It has received 11 citations till now. The article focuses on the topics: Dutch roll.

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

TL;DR: Hollkamp et al. as mentioned in this paper proposed a self-tuning piezoelectric Vibration Absorber for passive vibration suppression in wing-like composite structures.
Proceedings ArticleDOI

Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis - A State-of-the-Art

TL;DR: The state-of-the-art in the use of bifurcation and continuation methods for the analysis of aircraft trim and stability with a few illustrative examples are described.

Combat aircraft agility metrics - a review

TL;DR: In this review, agility metrics have been suitably classified, and the effects of advanced controls, such as thrust vectoring, and optimal maneuvers on combat performance, as suggested by agility metrics, have been investigated.
Proceedings ArticleDOI

Bifurcation Analysis of the Generic Transport Model with a view to Upset Recovery

TL;DR: In this article, the authors apply bifurcation theory to the Generic Transport Model (GTM) to investigate the effect of the aircraft elevator and throttle on the aircraft behavior, showing that aerodynamic stall negatively affects the lateral dynamics.
Journal ArticleDOI

Bifurcation analysis of inertia coupled roll manoeuvres of airplanes

TL;DR: In this article, the extended bifurcation analysis (EBA) technique has been proposed for the analysis of dynamical systems with constrained equilibrium states, and it has been shown that the EBA technique can be applied to the problem of dynamic systems with bounded equilibrium states.
References
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AUTO 2000 : CONTINUATION AND BIFURCATION SOFTWARE FOR ORDINARY DIFFERENTIAL EQUATIONS (with HomCont)

TL;DR: This is a guide to the software package AUTO for continuation and bifurcation problems in ordinary differential equations and the development of HomCont has much benefitted from various pieces of help and advice from, among others, W. W. Norton.
Journal ArticleDOI

Bifurcation Analysis of Nonlinear Aircraft Dynamics

TL;DR: In this article, a new approach for analyzing nonlinear and high-a dynamic behavior and stability of aircraft is presented, which involves the application of bifurcation analysis and catastrophe theory methodology to specific phenomena such as stall, departure, spin entry, flat and steep spin, nose slice, and wing rock.
Journal ArticleDOI

Introduction to Airborne Radar, 2nd ed.

Jon Rigelsford
- 01 Sep 2002 - 
Journal ArticleDOI

Application of Bifurcation Theory to the High-Angle-of-Attack Dynamics of the F-14

TL;DR: Bifurcation theory has been used to study the nonlinear dynamics of the F-14, and a simple feedback control system was designed to eliminate the wing rock and spiral divergence as mentioned in this paper.
Journal ArticleDOI

Application of bifurcation methods to nonlinear flight dynamics problems

TL;DR: In this paper, applications of global stability and bifurcational analysis methods are presented for different nonlinear flight dynamics problems, such as roll-coupling, stall, spin, etc.
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