Applications of bifurcation methods to F-18/HARV open-loop dynamics in landing configuration

Defence Science Journal

Volumn 52, Issue 2, 2002, Pages 103-115

  Sinha, Nandan Kumar ^a  

^a INDIAN INSTITUTE OF TECHNOLOGY BOMBAY   (India)

Author keywords

Aircraft instabilities prediction; Bifurcation methods; Fighter aircraft; Flight control; Flight instabilitics; Flight mechanics; Nonlinear aircraft dynamics; Nonlinear dynamics; Open loop dynamics; Standard bifurcation analysis; Wing rock motion

Indexed keywords

AIRCRAFT LANDING; BIFURCATION (MATHEMATICS); COMPUTER SIMULATION; FIGHTER AIRCRAFT; MANEUVERABILITY;

OPEN-LOOP DYNAMICS;

FLIGHT DYNAMICS;

EID: 0036531152     PISSN: 0011748X     EISSN: None     Source Type: Journal    
DOI: 10.14429/dsj.52.2155     Document Type: Article

References (16)

1. Bifurcation analysis of nonlinear aircraft dynamics
2. Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14
3. Bifurcation analysis of a highly augmented aircraft model
4. Using bifurcation methods to aid nonlinear dynamic inversion control law design
5. Application of bifurcation methods to nonlinear dynamics problems
6. Prevention of jump in inertia-coupled roll maneuvers of aircraft
7. Development of control schedules to modify spin behaviour
8. Analysis of longitudinal flight dynamics: A bifurcation-theoretic approach
9. Time-optimal lateral manoeuvers of an aircraft