Level flight trim and stability analysis using extended bifurcation and continuation procedure

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 6, 2001, Pages 1225-1228

  Ananthkrishnan, N ^a   Sinha, N K ^a  

^a INDIAN INSTITUTE OF TECHNOLOGY BOMBAY   (India)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BIFURCATION (MATHEMATICS); CONTACT ANGLE; MANEUVERABILITY; NONLINEAR CONTROL SYSTEMS;

FLIGHT CONTROL; FLIGHT INSTABILITIES; WING ROCK; YAW DEPARTURE;

FLIGHT DYNAMICS;

EID: 0035507945     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4839     Document Type: Article

References (10)

1. Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14
2. Prevention of jump in inertia-coupled roll maneuvers of aircraft
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 flight dynamics problems
6. Inertia-coupled coordinated roll maneuvers of airplanes
7. Multiple attractors in inertia-coupled velocity vector roll maneuvers of airplanes
8. Computation of flight mechanics parameters using continuation techniques
9. AUTO94: Software for continuation and bifurcation problems in ordinary differential equations
10. Time-optimal lateral maneuvers of an aircraft