Effects of rate limiting elements in flight control systems - A new PIO-criterion-Reference-Cited by-同舟云学术

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Effects of rate limiting elements in flight control systems - A new PIO-criterion

Published:1995-08-07 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Duda Holger

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-3204

Reference16 articles.

1. Induced Oscillations: Their Cause and Analysis", NORAIRReportNo. NOR-64-143,1964 2. McRuer, D.T. "Human Dynamics and Pilot

2. Neal, T.P., Smith, R.E. "A Flying Qualities Criterion for Design of Fighter Flight-Control Systems",AIAAPaper 70-927, 1971

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1. Adaptive Flight Control in the Presence of Limits on Magnitude and Rate;IEEE Access;2022

2. Effect of Actuator Saturation on Pilot-Induced Oscillation: A Nonlinear Bifurcation Analysis;Journal of Guidance, Control, and Dynamics;2021-05

3. PIO Engineering Prediction Methods and Verification of Airworthiness Compliance for Civil Aircraft;Lecture Notes in Electrical Engineering;2019

4. In-Flight Simulator VFW 614 ATTAS;In-Flight Simulators and Fly-by-Wire/Light Demonstrators;2017

5. Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings – A design perspective;Progress in Aerospace Sciences;2015-07

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