Now showing items 1-4 of 4
Computation of controllability regions for unstable aircraft dynamics.
(American Institute Aeronautics and Astronautics, 2004-01-01)
An active control approach to air vehicle design can significantly expand the flight envelope and improve vehicle performance characteristics. In some cases it can be attained by implementing the aerodynamically ...
Aircraft dynamics at high incidence flight with account of unsteady aerodynamic effects.
An adequate modelling of nonlinear and unsteady aerodynamics at high incidence flight is important for design of future agile and stealth fighters as well as for improved prediction of high angle of attack dynamics of ...
Computational framework for investigation of aircraft nonlinear dynamics.
A computational framework based on qualitative theory, parameter continuation and bifurcation analysis is outlined and illustrated by a number of examples for inertia-coupled roll maneuvers. The focus is on the accumulation ...