Department: History & Pakistan Studies
Extension Number: 824
Office Number: F-002

EDUCATION
PhD, History,
Middlesex University (London, UK)
MA, Religion,
Reformed Theological Seminary (Charlotte, NC, USA)
MS, Mathematics,
Ohio University (Athens, OH, USA)
BS, Mathematics,
Wheaton College (Wheaton, IL, USA)

BRIEF PROFILE
Dr. Norman has had an atypical career, having taught mathematics,computer science, theology, history, and philosophy in three differentcountries prior to Forman. Formerly he was a Senior Principal FlightControl Engineer at the Boeing Company where he designed controllaws for advanced technology aircraft, four of which were built andsuccessfully flight tested. His current interests are of an interdisciplinarynature, where the ideas of science, philosophy, history, and religionconverge.

RESEARCH & PUBLICATIONS
1.Saving the Church of England: John Edwards (1637-1716) asDissenting Conformer (Eugene, OR: Wipf & Stock, 2022)
2. with L.L. Berg et. al., VTOL UAV Concept Free-Flight Test Program,D6-70352TN, The Boeing Company, October 1991.
3.“Maneuver Enhancement and Gust Alleviation for the AFTI/F-111:Mode Development and Postflight Analysis”, Proceedings of AFTI/F-111Symposium (NASA Conference Publication 3055), April 1989.
4.with R.J. Hynes and D. Gangsaas, “An Integrated ManeuverEnhancement and Gust Alleviation Mode for the AFTI/F-111 MAWAircraft”, Proceedings, AIAA Conference on Guidance and Control,August 1983.
https://arc.aiaa.org/doi/abs/10.2514/6.1983-2217
5.with G.W. Hanks, et. al., Integrated Application of Active ControlsTechnology to an Advanced Subsonic Transport Project (NASA CR165631), October, 1981.
https://ntrs.nasa.gov/api/citations/19810011534/downloads/19810011534.pdf
6.Nonlinear Actuator Modeling for Efficient Time History Simulation, D6-51105TN, The Boeing Company, September 10, 1981.
7.A Survey of Model Reduction Techniques for Linear Dynamic Systems,D6-48901TN, The Boeing Company, February 12, 1981.
8.with D. Gangsaas and U. Ly, “Practical Gust Load Alleviation andFlutter Suppression Control Laws Based on LQG Methodology”,Proceedings of the AIAA 19th Aerospace Sciences Meeting, January 12-15, 1981.
https://arc.aiaa.org/doi/10.2514/6.1981-21
US PATENT
#4821981, April 18, 1989
with D. Gangsaas, “Maneuver Enhancement and Gust AlleviationSystem.”