A Learn-to-Fly Approach for Adaptively Tuning Flight Control Systems
Modal Filtering for Control of Flexible Aircraft
Simulation Evaluation of Pilot Inputs for Real Time Modeling During Commercial Flight Operations
Position Corrections for Airspeed and Flow Angle Measurements on Fixed-Wing Aircraft
Flight Test Results on the Stability and Control of the F-15 Quiet Spike(TradeMark) Aircraft
Design and Control of an Experimental Tilt-Wing Aircraft
In-Trail Procedure Air Traffic Control Procedures Validation Simulation Study
Design of Low Complexity Model Reference Adaptive Controllers
An Adaptive Control Technology for Safety of a GTM-like Aircraft
Effects of the 8 psia / 32% O2 Atmosphere on the Human in the Spaceflight Environment
Trajectory Specification Applied to Terminal Airspace
Information requirements for guidance and control systems
Basic studies in space vehicle attitude control Ninth semiannual status report
Flight Dynamics Analysis Branch End of Fiscal Year 2005 Report
Data requirements for in-flight synthesis and multiple blender studies
Crew Procedures for Continuous Descent Arrivals Using Conventional Guidance
Studies of manual control systems progress report no. 7, 19 jan. - 18 apr. 1965
Aeroservoelastic Stability Analysis of the X-43A Stack
Implementation of an Adaptive Controller System from Concept to Flight Test
Stability and Control Analysis of the F-15B Quiet SpikeTM Aircraft
Tailored Excitation for Frequency Response Measurement Applied to the X-43A Flight Vehicle
Vertical Motion Simulator Experiment on Stall Recovery Guidance
Guidance and Control of an Autonomous Soaring UAV
Guidance and Control of an Autonomous Soaring UAV
Autonomous Airborne Refueling Demonstration, Phase I Flight-Test Results
Magnetic attitude control of rigid, axially symmetric, spinning satellites in circular earth orbits
Electro-pneumatic actuation system Interim technical report
Study of optimal and adaptive control theory Final report, May 1964 - Jun. 1966
A guide of the application of the liapunov direct method to flight control systems
Research on the design of adaptive control systems, volume 2 Final report
A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design
Manual Manipulation of Engine Throttles for Emergency Flight Control
Control Laws for a Wind Tunnel Free-Flight Study of a Blended-Wing-Body Aircraft
Analysis and design of space vehicle flight control systems. Volume XV - Elastic body equations
The case for inherent stability of helicopters
Bias Momentum Sizing for Hovering Dual-Spin Platforms