MINIGUIDE - A SIMPLIFIED ATTITUDE CONTROL FOR SPINSTABILIZED VEHICLES
A TECHNIQUE FOR OPTIMUM FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIES
THEORETICAL AND PRACTICAL ASPECTS OF SOLAR PRESSURE ATTITUDE CONTROL FOR INTERPLANETARY SPACECRAFT
Active Control of Separation From the Flap of a Supercritical Airfoil
Post-Stall Aerodynamic Modeling and Gain-Scheduled Control Design
Mitigating Motion Base Safety Issues: The NASA LaRC CMF Implementation
TECHNICAL ADVANTAGES OF FLUID POWER
Advanced Video Guidance Sensor and Next Generation Autonomous Docking Sensors
Pathway Design Effects on Synthetic Vision Head-Up Displays
APPLICATION OF SELF-ADAPTIVE CONTROL TECHNIQUES TO THE FLEXIBLE SUPERSONIC TRANSPORT
Design of a Multi-mode Flight Deck Decision Support System for Airborne Conflict Management
Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System
Adaptive Spacecraft Attitude Control With Application to Space Station
Attitude Control for an Aero-Vehicle Using Vector Thrusting and Variable Speed Control Moment Gyros
Dynamic Stall Measurements and Computations for a VR-12 Airfoil with a Variable Droop Leading Edge
Flight Test of the F/A-18 Active Aeroelastic Wing Airplane
Free-to-Roll Investigation of Uncommanded Lateral Motions for an Aircraft with Vented Strakes
Dynamics Modeling and Simulation of Large Transport Airplanes in Upset Conditions
Control Reallocation Strategies for Damage Adaptation in Transport Class Aircraft
THE DESIGN OF THE ATTITUDE CONTROL SYSTEM FOR THE ORBITING GEOPHYSICAL OBSERVATORY
Free-to-Roll Investigation of Uncommanded Lateral Motions for an Aircraft With Vented Strakes
Wake Vortex Tracking Using a 35 GHz Pulsed Doppler Radar
A Fast-Time Simulation Environment for Airborne Merging and Spacing Research
Overview of Active Flow Control Actuator Development at NASA Langley Research Center
Cartesian-Grid Simulations of a Canard-Controlled Missile with a Free-Spinning Tail
AN APPLICATION OF TIME OPTIMAL CONTROL TO A FLEXIBLE LAUNCH VEHICLE
Overview of Intelligent Systems and Operations Development
Cost Estimation and Control for Flight Systems
Visualizing Decision-making Behaviours in Agent-based Autonomous Spacecraft
An Adaptive Critic Approach to Reference Model Adaptation
Intelligent Control Approaches for Aircraft Applications
18-Degree-of-Freedom Controller Design for the ST7 Disturbance Reduction System
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
Flight Control System Development for the BURRO Autonomous UAV
Adaptive Admittance Control: An Approach to Explicit Force Control in Compliant Motion
Flight Test Experience With an Electromechanical Actuator on the F-18 Systems Research Aircraft
Robust Load-Sharing Control of Spacecraft Formations
Use of Individual Flight Corridors to Avoid Vortex Wakes
Optimal Aircraft Control Upset Recovery With and Without Component Failures
Numerical Simulation of Rolling-Airframes Using a Multi-Level Cartesian Method
A Roadmap for Aircraft Engine Life Extending Control