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Excessive roll damping can cause roll ratchet

  • Published:1983-05 Issue:3 Volume:6 Page:218-219
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Chalk C.R.1

Affiliation:

1. Arvin/Calspan Corporation, Buffalo, New York

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

Reference5 articles.

1. 2Harper, R.P. Jr. "In-Flight Simulation of the Lateral-Directional Handling Qualities of Entry Vehicles," Calspan Rept. TE-1243-F-2, Feb.1961.

2. 4Smith, R.E. "Evaluation of F-18A Approach and Landing Flying Qualities Using an In-Flight Simulator," Calspan Rept. 6241-F-l, Feb.1979.

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1. Handling Qualities Criteria for Roll Control of Highly Augmented Aircraft;Journal of Guidance, Control, and Dynamics;2003-11

2. Unified Approach for Roll Ratcheting Analysis;Journal of Guidance, Control, and Dynamics;1999-09

3. A biomechanical pilot model for prediction of roll ratcheting;24th Atmospheric Flight Mechanics Conference;1999-08-09

4. Theory for Roll-Ratchet Phenomenon in High-Performance Aircraft;Journal of Guidance, Control, and Dynamics;1998-01

5. Unified Theory for Aircraft Handling Qualities and Adverse Aircraft-Pilot Coupling;Journal of Guidance, Control, and Dynamics;1997-11
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