Existence of oscillatory solutions along the path of longitudinal flight equilibriums of an unmanned aircraft, when the automatic flight control system fails

Author:

Balint St.,Balint A.M.,Kaslik E.

Publisher

Elsevier BV

Subject

Applied Mathematics,Analysis

Reference15 articles.

1. R.K. Mehra, R.K. Prasanth, Bifurcation and limit cycle analysis of nonlinear pilot induced oscillations, 1998, AIAA-98-4249

2. Unified pilot-induced oscillation theory, Wright-Patterson AFB, Ohio, 1996, vols. I–IV, WL-TR-96, pp. 3028–3031

3. A. Ionita, A. Halanay, Delay induced oscillations, 1977, AIAA-97-3502

4. B.A. Kish et al., A limited flight test investigation of pilot-induced oscillation due to rate limiting, 1997, AIAA Paper 97-3703

5. Pilot-induced oscillation analysis and prediction with actuator rate limiting;Klyde;J. Guidance Control Dynamics,1997

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