Synonyms were used for:
Standsicherheit
Search without synonyms:
keywords:(Standsicherheit)
Investigation of Downwash and Wake Characteristics at a Mach Number of 1.53 I : Rectangular Wing
Dynamic instability : automobiles, aircraft, suspension bridges
Elastic stability of a slender bar under dynamic loads
Methods for Obtaining Desired Helicopter Stability Characteristics
Method of calculating the lateral motions of aircraft based on the Laplace transform
Variable Geometry Aircraft Pylon Structure and Related Operation Techniques
Strategies for Uncertainty Modeling and Optimization Under Uncertainty
Initial Assessment of Stability and Controllability in the Early Stage of Combat Aircraft Design
Design of a Collocation-Based Active Flutter Suppression Control Law for the IAWTM Wind Tunnel Model
Low-speed wind-tunnel investigation of tension-structure parawings
A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle
STATIC STABILITY AND CONTROL OF HYPERSONIC GLIDERS
A system for varying the stability and control of a deflected-jet fixed-wing vtol aircraft
Gust Alleviation Using Direct Gust Measurement
Benchmark Active Controls Technology (BACT) Wing CFD Results
A describing-function analysis of the stability of a launch vehicle with nonlinear thrust vectoring
Flight Test of an Adaptive Configuration Optimization System for Transport Aircraft
X-33 Attitude Control Using the XRS-2200 Linear Aerospike Engine
Emergency flight control system using one engine and fuel transfer
Technology Integration (Task 20) Aeroservoelastic Modeling and Design Studies
Investigation of Dynamic Flight Maneuvers With an Iced Tailplane
X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes
Ascent, Transition, Entry, and Abort Guidance Algorithm Design for the X-33 Vehicle
Stability and control considerations for STOL AIRCRAFT.
Effect of product of inertia on lateral stability
Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
Trajectory Generation for Distributed Electric Propulsion Vehicles with Propeller Synchronization
X-33 Ascent Flight Controller Design by Trajectory Linearization: A Singular Perturbational Approach
Distortion Tolerant Control Demonstrated in Flight
An Overview of Controls and Flying Qualities Technology on the F/A-18 High Alpha Research Vehicle
Emergency Flight Control Using Only Engine Thrust and Lateral Center-of-Gravity Offset: A First Look
A survey of stability analysis techniques for automatically controlled aircraft
L1 Adaptive Control with Switched Reference Models: Application to Learn-to-Fly
Rotorcraft control system design for uncertain vehicle dynamics using quantitative feedback theory
Time-optimal reorientation maneuvers for a combat aircraft
Computation of maximized gust loads for nonlinear aircraft using matched-filter-based schemes