1. “Application of Nonlinear System Inverses to Automatic Flight Control Design System Concepts and Flight Evaluation,”;Meyer,1981
2. G. Meyer and W. Wherend, “DHC-6 Flight Tests of the Total Automatic Flight Control System (TAFCOS) Concept on a DHC-6 Twin-Otter Aircraft,” NASA TP-1513, 1980.
3. G. Smith and G. Meyer, “Application of the Concept of Dynamic Trim Control to Automatic Landing of Carrier Aircraft,” NASA TP-1512, 1980.
4. G. Smith and G. Meyer, “Total Aircraft Flight Control System—Balanced Open and Closed Loop Control with Dynamic Trim Maps,” Proceedings of the 3rd Digital Avionics Systems Conference, Fort Worth, Texas, Nov. 1979.
5. G. Smith and G. Meyer, “Application of Dynamic Trim Control and Nonlinear System Inverses to Automatic Control of a Vertical Attitude Takeoff and Landing Aircraft,” Proceedings of the 4th Digital Avionics Systems Conference, St. Louis, Missouri, Nov. 1981.