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Investigation of Nonlinear Controller for Propulsion Controlled Aircraft
Measurement of the Yawing Moment of Inertia of an Aircraft (Hp115) IN Flight
Impact of Flying Qualities on Helicopter Operational Agility
Design of Low Complexity Model Reference Adaptive Controllers
Electromechanical flight actuators for advanced flight vehicles
Hybrid Lta Vehicle Controllability as Affected by Buoyancy Ratio
Applications of Flight Control System Methods to an Advanced Combat Rotorcraft
Comparison of Low-Speed Handling Qualities in Ground-Based and In-Flight Simulator Tests
Helicopter Roll Control Effectiveness Criteria Program Summary
Vstol Aircraft Stability and Control Experience from Methods and Results of Do 31 Flight Tests
Multi-Feeder Protection System with Hybrid Circuit Breakers for MVDC Grids
Steuerung und Lademanagement eines Brennstoffzellen-basierten Hybridsystems
Low-Lift-TO-Drag-Ratio Approach and Landing Studies Using a Cv-990 Airplane
Simulator Evaluation of a Remotely Piloted Vehicle Lateral Landing Task Using a Visual Display
Flight Validation of a Handling Qualities Metric for a Damaged Aircraft
Flight Investigation of the Effect of Tail Boom Strakes on Helicopter Directional Control
Determination of Dynamic Characteristics from Flight Test Data
Analysis of Asymmetric Aircraft Aerodynamics Due to an Experimental Wing Glove
X-31A High Angle of Attack and Initial Post Stall Flight Testing
Pilot Control Through the Tafcos Automatic Flight Control System
Analyses and Tests of the B-1 Aircraft Structural Mode Control System
The Influence of Running Propellers on Low Speed Longitudinal Static Stability Trim Curves
Demonstration of Frequency-Sweep Testing Technique Using a Bell 214-St Helicopter
Preliminary Design Study of a Lateral-Directional Control System Using Thrust Vectoring
Development of Control Laws for a Flight Test Maneuver Autopilot for an F-15 Aircraft
Role of Handling Qualities Specifications in Flight Control System Design
Factors Affecting Handling Qualities of a Lift-Fan Aircraft During Steep Terminal Area Approaches
Generic Inner-Loop Control Law Structure for Six-Degree-of-Freedom Conceptual Aircraft Design