Nonlinear Prefilter to Prevent Pilot-Induced Oscillations due to Actuator Rate Limiting-Reference-Cited by-同舟云学术

Nonlinear Prefilter to Prevent Pilot-Induced Oscillations due to Actuator Rate Limiting

Published:2002-07 Issue:4 Volume:25 Page:740-747
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Liebst Brad S.¹,Chapa Michael J.¹,Leggett David B.¹

Affiliation:

1. U.S. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433-7765

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.4941

Reference9 articles.

1. Handling Criteria

2. Chapa, M. “A Nonlinear Pre-Filter To Prevent Departure and/or Pilot-Induced Oscillations (PIO) Due To Actuator Rate Limiting,” M.S. Thesis, AFIT/GAE/ENY/99M-01, Graduate School of Engineering, Air Force Inst. of Technology (AU), Wright-Patterson AFB,OH, March 1999.

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