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title: aerospace actuator 1
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title: Aerospace Actuators 1
Doubly Coupled Antagonistic Shape Memory Alloy Actuator for Morphing Wing
Shape memory alloy (SMA) wires have received considerable attention for use in actuators in morphing wings. This
...Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults
During the aerospace missions for the on-orbiting spacecraft, actuator faults are frequently encountered such
...Distributed FTCC of Multi-UAVs Under Actuator Fault and Input Saturation
L1 adaptive fault-tolerant control of stratospheric airships
Bombardier Global 7500 Fatigue Test Cycle Rate Commissioning to ¼ Life
The second wind-tunnel test of DLR’s multiple swashplate system
Boundary-Layer Transition Control by Plasma Crossflow Reduction in Swept Wing
Fault-Tolerant Control on a UH-60 Black Hawk helicopter using horizontal stabilator
Study on Aerodynamic Characteristics of “Propeller/Wing” System with Overset Mesh Method
Fault Tolerant Control of Large Civil Aircraft
Experimental investigation and design of a shape-variable compressor cascade
Research on the Aerodynamic Failure Load for Civil Aircraft
Signal-Dependent Uncertainty Compensation: A General Framework
The process of modeling of SJAs at low AoA [1, 2] is very different from that at high
...NN-Based High-Order Adaptive Compensation Framework for Signal Dependencies
Attitude Control on GRACE Follow-On: Experiences from the First Years in Orbit
Adaptive Compensation at High Angles of Attack
In-Orbit Experience of the Gaia and LISA Pathfinder Cold Gas Micro-propulsion Systems
Adaptive Compensation at Low Angles of Attack: Nonlinear Aircraft Model
Hinge Moment Characterization of All Movable Control Surface
Evaluation of the Reduction in the Performance of a UAV
Industrial Practices in Fault Tolerant Control
Variational Problem of Vibration Suppression for Thermoelastic Axially Moving Web
Smart Morphing and Sensing for the Wings of the Future
Analysis of a multi-functional high-lift system driven by an active differential gear box
Structural concept of an adaptive shock control bump spoiler
Pressure Amplification Coefficient of the “Nozzle-Flap” Transducer
The principle of operation of automatic control system of hydraulic actuator based on hydraulic measuring
...Robust and Adaptive Control with Output Feedback