Related Publications:
Klyde, D. H., A. K. Lampton, N. D. Richards, B. Cogan, “Flight Test Evaluation of a Loss of Control Mitigation System,” J. of Guidance, Control, and Dynamics, Vol. 40, No. 4, April 2017, pp. 981-997.
Klyde, D. H., P. C. Schulze, R. Mello, and D. G. Mitchell, “Assessment of a Scalogram-Based PIO Metric with Flight Test Data,” AIAA-2017-1641 presented at the Science and Technology Forum and Exposition 2017: AIAA Atmospheric Flight Mechanics Conference, Grapevine, TX, Jan. 9–13, 2017.
Mitchell, D. G., and D. H. Klyde, “Finding Commonality in the Uncommon: Encountering PIO in Flight Test,” 46th Society of Flight Test Engineers International Symposium, Lancaster, CA, 14-17 Sept. 2015.
Klyde, D. H., P. C. Schulze, and P. M. Thompson, “Exposing Unique Pilot Behaviors from Flight Test Data,” AIAA Paper No. 2015-0239 presented at the Science and Technology Forum and Exposition 2015: AIAA Atmospheric Flight Mechanics Conference, Kissimmee, Florida, January 5-9, 2015.
D. H. Klyde, C. Y. Liang, N. Richards, B. Cogan, “Use of Active Inceptor Cueing to Mitigate Pilot-Vehicle System Loss of Control,” AIAA Paper No. 2012-4765 presented at the Guidance, Navigation, and Control Conference, Minneapolis, MN, 13-16 Aug. 2012.
D. H. Klyde, C. Y. Liang, D. J. Alvarez, N. Richard, R. J. Adams, and B. Cogan, “Mitigating Unfavorable Pilot Interactions with Adaptive Controllers in the Presence of Failures/Damage,” AIAA Paper to be presented at Atmospheric Flight Mechanics Conference, Portland, OR, 8-11 August, 2011.
D. H. Klyde and C.-Y. Liang, Ph.D., “Flight Assessment of Pilot Behavior with Smart-Cue and Smart-Gain Concepts Active,” AIAA 2009-5606 presented at AIAA Atmospheric Flight Mechanics Conference, Chicago, IL, August 10, 2009.
D. H. Klyde and C.-Y. Liang, Ph.D., “Approach and Landing Flight Evaluation of Smart-Cue and Smart-Gain Concepts,” Journal of Guidance, Control, and Dynamics, vol. 32, no. 4, pp. 1057-1070, 2009.
D. G. Mitchell and D. H. Klyde, “Identifying a Pilot-Induced Oscillation Signature: New Techniques Applied to Old Problems,” Journal of Guidance, Control, and Dynamics, vol. 31, no. 1, pp. 215-224, 2008.
D. H. Klyde and D. T. McRuer, “Smart-Cue and Smart-Gain Concepts Development to Alleviate Loss of Control,” Journal of Guidance, Control, and Dynamics, vol. 32, no. 5, pp. 1409-1417, 2009.
D. G. Mitchell and D. H. Klyde, “Testing for Pilot-Induced Oscillations,” AIAA 2005-5811 presented at AIAA Atmospheric Flight Mechanics Conference and Exhibit, San Francisco, CA, August 15-18, 2005.
D. H. Klyde and D. G. Mitchell, “A PIO Case Study – Lessons Learned through Analysis,” AIAA 2005-5813 presented at AIAA Atmospheric Flight Mechanics Conference and Exhibit, San Francisco, CA, August 15-18, 2005.
D. H. Klyde and D. G. Mitchell, “Recommended Practices for Exposing Pilot-Induced Oscillations or Tendencies in the Development Process,” AIAA 2004-6810 presented at USAF Developmental Test and Evaluation Summit, Woodland Hills, CA, November 16-18, 2004.
D. H. Klyde and D. G. Mitchell, “Investigating the Role of Rate Limiting in Pilot-Induced Oscillations,” Journal of Guidance, Control, and Dynamics, vol. 27, no. 5, pp. 804-816, 2004.
D. G. Mitchell, V. Sahasrabudhe, and D. H. Klyde, “Determining Bandwidth in the Presence of Nonlinearities,” AIAA 99-0639presented at AIAA 37th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 11-14, 1999.
D. H. Klyde, D. G. Mitchell, and K. J. Latimer, “Development of the Probe-and Drogue Handling Qualities Demonstration Maneuver,” Journal of Guidance, Control, and Dynamics, vol. 22, no. 4, pp. 528-535, 1999.
D. H. Klyde and D. G. Mitchell, “Extraction of Pilot-Vehicle Characteristics In the Presence of Rate Limiting,” AIAA 99-1069 presented at AIAA 37th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 11-14, 1999.
D. G. Mitchell and D. H. Klyde, “A Critical Examination of PIO Prediction Criteria,” AIAA-98-4335 presented at AIAA Atmospheric Flight Mechanics Conference and Exhibit, Boston, MA, August 10-12 1998.
D. H. Klyde, D. T. McRuer, and T. T. Myers, “Pilot-Induced Oscillation Analysis and Prediction with Actuator Rate Limiting,” Journal of Guidance, Control, and Dynamics, vol. 20, no. 1, pp. 81-89, 1996.
D. G. Mitchell, B. L. Aponso, and D. H. Klyde, “Feel Systems and Flying Qualities,” AIAA 95-3425 presented at AIAA Atmospheric Flight Mechanics Conference, Baltimore, MD, August 7-10, 1995.
D. G. Mitchell, R. H. Hoh, B. L. Aponso, and D. H. Klyde, “The Measurement and Prediction of Pilot-in-the-Loop Oscillations,” AIAA-1994-3670 presented at AIAA Guidance, Navigation and Control Conference, Scottsdale, AZ, August 1-3, 1994.