Structural Technology Evaluation and Analysis Program (STEAP). Delivery Order 0037: Prognosis-Based Control Reconfiguration for an Aircraft With Faulty Actuator to Enable Performance in a Degraded State

doi 10.21236/ada534168
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Defense Technical Information Center

Related search

Fault-Tolerant Control Allocation With Actuator Dynamics: Finite-Time Control Reconfiguration

2014English

Third Order Sliding Mode Control With a Predefined Convergence Time: Application to an Electropneumatic Actuator

2017English

An Active Mass Damper Using Rotating Actuator for Structural Vibration Control

Advances in Mechanical Engineering
Mechanical Engineering
2016English

Using Partial Reconfiguration and Message Passing to Enable FPGA-Based Generic Computing Platforms

International Journal of Reconfigurable Computing
HardwareArchitecture
2012English

Predictive Control Using an FPGA With Application to Aircraft Control

IEEE Transactions on Control Systems Technology
ControlSystems EngineeringElectricalElectronic Engineering
2014English

Evaluation of Management System Effectiveness in the Preparation of the Aircraft for Flight in Faulty Conditions

Transport and Aerospace Engineering
2015English

Adaptive Neural Control Based on High Order Integral Chained Differentiator for Morphing Aircraft

Mathematical Problems in Engineering
MathematicsEngineering
2015English

Performance-Based Sensor Reconfiguration for Fault-Tolerant Control of Uncertain Spatially Distributed Processes

IFAC Proceedings Volumes
2014English

Augmenting L1 Adaptive Control of Piecewise Constant Type to a Fighter Aircraft. Performance and Robustness Evaluation for Rapid Maneuvering.

2012English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy