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PILOT-INDUCED OSCILLATIONS: From the Wright Flyer to Fly-by-Wire
|  | A two-day professional development short course presented by...
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| David G. Mitchell Technical Director Hoh Aeronautics, Inc.
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| David H. Klyde Principal Research Engineer Systems Technology, Inc.
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PILOT-INDUCED OSCILLATIONS (PIO) are rare, unexpected, and unintended excursions in aircraft attitude and flight path caused by anomalous interactions between the aircraft and pilot. They have occurred at some time in the development cycle for just about every new air vehicle design. Catastrophic events that lead to mishaps cost time, money, and sometimes lives. With the advent of modern flight control systems, the potential for catastrophic PIO is on the rise.
In this two-day short course, the phenomenon of PIO will be examined from its origins to today's events. With practical examples from flight research, flight test, and operational experience, the speakers identify the myriad causes of PIO and describe the cures available to the design engineer.
The course is intended for a broad audience including program managers, controls and flight test engineers, and pilots. At the end of the course, the attendee will be familiar with:
- Causes of the most publicized PIOs
- Methods for their prevention by design and prediction by analysis
- Simulation and flight test techniques to expose PIO tendencies
- Tools for real-time monitoring
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Day 1 Topics:
- What Are Pilot-Induced Oscillations?
- A Brief History of PIO (featuring a comprehensive collection of PIO Videos)
- Aircraft Dynamics and Augmentation
- Pilot Dynamics in Closed-Loop Control
- Triggers
- The Categories and Causes of PIO
- Rating the PIO
- PIO Flight Research Programs
- Designing Category I PIO Resistant Aircraft
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 | Day 2 Topics:
- Designing Category I PIO Resistant Aircraft (continued): A Comparative Evaluation of Category I Criteria
- Designing Category II PIO Resistant Aircraft
- Detection and Prevention in Real-Time
- Testing for PIO
- PIO Case Studies (including X-15, F-14, V-22, F/A-18F, T-45, & B777)
- Summary and Conclusions
- A Hands-On Experience: Desktop Simulation of PIO
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The PIO Short Course has been taught on site to the following organizations:
Boeing Phantom Works | Long Beach, CA | April 2003 | Naval Air Systems Command | NAS Patuxent River, MD | February 2004 | Boeing Integrated Defense Systems | Philadelphia, PA | March 2004 | US Air Force Flight Test Center | Edwards AFB, CA | December 2004 | Bell Helicopter Textron, Inc. | Arlington, TX | July 2005 | US Air Force Flight Test Center | Edwards AFB, CA | August 2005 | Sikorsky Aircraft Co. | Stratford, CT | September 2005 |
ABOUT THE SPEAKERS:
DAVID G. MITCHELL is Technical Director for Hoh Aeronautics, Inc., in Lomita, CA. In his 27 years in aerospace, he has co-authored 50 technical papers and more than 50 technical reports, and has contributed articles to two textbooks. A report on PIO for the U.S. Air Force in 2000 is used as a reference source by military and civilian agencies, and is considered a "must read" on the topic by engineers at the Federal Aviation Administration. Hoh Aeronautics, Inc.
DAVID H. KLYDE is a Principal Research Engineer for Systems Technology, Inc., in Hawthorne, CA. In his more than 18 years of experience, he has worked on projects involving handling of both air and ground vehicles. He was the project engineer for STI on the USAF Unified PIO Theory program that investigated the role of actuator rate limiting as a causal factor in PIO. He was also project engineer on a recent program to identify the causes of, and develop cures for, PIO during landing rollout on the Navy's current jet trainer. For scheduling and course registration information, please contact
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310-679-2281, ext. 27
Download the instructors' recent papers on PIO: Systems Technology, Inc. Publications
Systems Technology, Inc. 13766 S. Hawthorne Blvd. Hawthorne, CA 90250
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