Subject
Applied Mathematics,Analysis
Reference25 articles.
1. R. Mehra, R. Prasanth, Bifurcation and limit cycle analysis of nonlinear pilot induced oscillations, in: AIAA Atmospheric Flight Mechanics Conference and Exhibit, Boston, MA, Aug. 10–12, 1998, Collection of Technical Papers.
2. Unified Pilot Induced Oscillation Theory, vols. I–IV, WL-TR-96: 3028–3031, Wright Patterson AFB, Ohio, 1996.
3. B. Kish, W.M. III, A. Remaly, J. Seo, J. Kromberg, R. Cabiati, A limit flight test investigation of pilot induced oscillation due to rate limiting, in: Proceedings of the AIAA Guidance, Navigation, and Control Conference, New Orleans, LA, 11–13 August 1997, No. AIAA-97-3703, pp. 1332–1341.
4. Pilot induced oscillation analysis and prediction with actuator rate limiting;Klyde;J. Guid. Control Dyn.,1997
5. R. Mehra, W. Kessel, J. Carroll, Global stability and control analysis of aircraft at high angles of attack, ONR-CR215-248-1, vols. 1–4.