Study-fluid flight path control system final report
The design of a large angle three-axis attitude servomechanism for spacecraft
Design Requirements for Unmanned Rotorcraft Used in Low-Risk Concepts of Operation
Pilot Comments for High Speed Research Cycle 3 Simulations Study (LaRC.1)
Pilot re-entry guidance and control
Control-System Techniques for Improved Departure/Spin Resistance for Fighter Aircraft
Identification of Low Order Equivalent System Models From Flight Test Data
Advanced High-Lift Leading-Edge (AHLLE) Technologies for Laminar Wings
Analysis and design of space vehicle flight control systems. Volume XIII - Adaptive control
Airfoil Dynamic Stall and Rotorcraft Maneuverability
Performance Modeling of a Pilot in a Free Flight Mode