230.548 People
De Visser, Cornelis
Delft University of Technology
in Cooperation with on an Cooperation-Score of 37%
Topics
- laser
- beltway
- data
- simulation
- frequency domain analysis
- camera
- fuselage
- filter
- warehousing
- aerodynamic
- consensus
- barge
- tunnel
- control device
- wind tunnel
- gust
- excitation
- linear regression analysis
- jet propelled aircraft
- intelligent control system
- COVID-19
- dynamic load
- vibrometer
- aircraft
- weight
- perturbation
- autocorrelation
- boundary layer separation
- gyroscope
- aerospace material
- surveillance
- noise
- machinery
- data file
- machine learning
- system of measurement
- pipeline
- laboratory
- forecasting
- reconstruction
- hub
- submarine
- virtual reality
- triangulation
- stereoscopic camera
- crash
- flight
- protection
- database
- assessment
- aircraft pilotage
- maintenance
- feedback control
- vibration
- sensor
- optimization
- performance evaluation
- particle beam
- train consist
- dynamic model
- impurity
- law
- stiffness
- sliding mode control
- actuator
- actuating system
- strain gage
- accelerometer
- design method
- flexible structure
- smart structure
- validation
- ice
- bottleneck
- constraint
- iterative method
- spline
- acceleration
- frequency response
- calibration
- system design
- flight control system
- transfer function
- angular acceleration
- information retrieval
- collapse
- adaptive control
- minimization
- curvature
- trailing edge
- superelevation
- atmospheric turbulence
- turbulence
- perception
- behavior
- safety
- complex system
- axis
- sensitivity
- flight test
- visualization
- vehicle
- modeling
- control system
- specification
- crop
- supervisor
- detection and identification
- trajectory
- profit
- trajectory control
- modernization
- drone
- velocity
- prevention
- aerospace engineering
- kinematics
- human body mass
- aerodynamic force
- monitoring
- nonlinear system
- aileron
- urban area
- burlap
- flight path
- civil aircraft
- benchmark
- engine
- airplane
- uncertainty
- automatic pilot
- rudder
- theorem
- air traffic controller
- decomposition
- wind
- heart
- density
- prototype
- process control
- supporting
- property
- mathematical model
- food
- show 114 more
Publications
- 2021Adaptive State Estimation and Real-Time tracking of Aeroelastic Wings with Augmented Kalman filter and Kernelized Correlation Filtercitations
- 2021Developing the Model Reduction Framework in High Frame Rate Visual Tracking Environment
- 2021Adaptive real-time clustering method for dynamic visual tracking of very flexible wings
- 2020Parallel Real-Time Tracking and 3D Reconstruction with TBB for Intelligent Control and Smart Sensing Frameworkcitations
- 2020Database-driven Safe Flight Envelope Protection for Impaired Aircraft
- 2020Design and Real-Time Implementation of a Vision-Based Adaptive Model-Free Morphing Wing Motion Control Method [PPT]
- 2019Distributed approach for aerodynamic model identification of the ice aircraft using the alternating direction method of multipliers in combination with simplotope b-splines
- 2018Characterising Angular Accelerometer Calibration Setup Disturbance Using Box–Jenkins Method
- 2018Online aircraft damage case identification and classification for database information retrieval
- 2018Effects of structural failure on the safe flight envelope of aircraftcitations
- 2018Active gust load alleviation of high-aspect ratio flexible wing aircraftcitations
- 2018Multivariate spline-based adaptive control for high performance aircraft in the presence of atmospheric turbulence
- 2018Aircraft damage identification and classification for database-driven online flight-envelope predictioncitations
- 2018Safe Exploration Algorithms for Reinforcement Learning Controllerscitations
- 2017Investigating cross-axis sensitivity andmisalignment in an angular accelerometermeasurement unit
- 2017Investigating Cross-Axis Sensitivity and Misalignment in an Angular Accelerometer Measurement Unitcitations
- 2017Flight Testing and Preliminary Analysis for Global System Identification of Ornithopter Dynamics Using On-board and Off-board Datacitations
- 2017Further results on the development of a novel VTOL aircraft, the Anuloid. Part II: Flight mechanics
- 2017Aviate, Navigate: Functional Visualizations of Asymmetric Flight Envelope Limitscitations
- 2017Aircraft damage identification and classification for database-driven online safe flight envelope prediction
- 2016A time-scale separation approach for time-varying model identification of a flapping-wing micro aerial vehiclecitations
- 2016Motion Simulator 2-Axis Input Design for Angular Accelerometer Calibrationcitations
- 2016Modelling an angular accelerometer using frequency-response measurementscitations
- 2016Time-varying model identification of flapping-wing vehicle dynamics using flight datacitations
- 2016Motion simulator 2-axes input design for angular accelerometer calibration
- 2016Aerodynamic model identification of a clap-and-fling flapping-wing MAV: A comparison between quasi-steady and black-box approachescitations
- 2016Piloted simulator evaluation of a model-independent fault-tolerant flight control system
- 2016Multivariate spline-based adaptive control of high-performance aircraft with aerodynamic uncertaintiescitations
- 2016Online physical model identification for database-driven safe flight envelope prediction of damaged aircraft
- 2016Nonlinear aircraft attitude and heading reference system failure detection and identification
- 2016Adaptive incremental backstepping flight control for a high-performance aircraft with uncertaintiescitations
- 2016Distance-fields-over-grids method for aircraft envelope determinationcitations
- 2016Nonlinear aircraft sensor fault reconstruction in the presence of disturbances validated by real flight datacitations
- 2016Online safe flight envelope prediction for damaged aircraft: A database-driven approach
- 2016Aircraft Fault-Tolerant Trajectory Control Using Incremental Nonlinear Dynamic Inversioncitations
- 2016Three-Dimensional Velocity Obstacle Method for Uncoordinated Avoidance Maneuvers of Unmanned Aerial Vehiclescitations
- 2016Distance Fields Over Grids Method for Aircraft Envelope Determinationcitations
- 2015Effects of eigenmodes, forward velocity and flapping frequency in force generation mechanisms of a flapping-wing mav
- 2015Data-informed quasi-steady aerodynamic model of a clap-and-fling flapping wing MAV
- 2015A high-precision position-based calibration table as the reference for angular accelerometer calibration experiment
- 2015Rigid-body kinematics versus flapping kinematics of a flapping wing micro air vehiclecitations
- 2015A framework for calibrating angular accelerometers using a motion simulatorcitations
- 2015Development of a new method for calibrating an angular accelerometer using a calibration tablecitations
- 2015Distance fields over grids method for aircraft envelope determination
- 2015Nonlinear aircraft sensor fault reconstruction in the presence of disturbances validated by real flight datacitations
- 2015Selective velocity obstacle method for deconflicting maneuvers applied to unmanned aerial vehiclescitations
- 2015Distance fields over grid method for aircraft envelope determinationcitations
- 2015Aircraft inertial measurement unit fault identification with application to real flight datacitations
- 2015Nonlinear and fault-tolerant flight control using multivariate splinescitations
- 2014Tethered vs. free flight force determination of the delfly II flapping wing micro air vehiclecitations
- 2014On the development of the Anuloid, a disk-shaped VTOL aircraft for urban areascitations
- 2014Rigid vs. flapping: The effects of kinematic formulations in force determination of a free flying flapping wing micro air vehiclecitations
- 2014Exploring Adaptive Incremental Backstepping using Immersion and Invariance for an F-16 aircraftcitations
- 2014Nonlinear Multivariate Spline-Based Control Allocation for High-Performance Aircraftcitations
- 2013Linear aerodynamic model identification of a flapping wing MAV based on flight test datacitations
- 2013Controlled flight maneuvers of a Flapping Wing Micro Air Vehicle: a step towards the Delfly II identificationcitations
- 2013Controlled Flight Maneuvers Of A Flappingwing Micro Air Vehicle: A step towards the delfly II identification
- 2013Modelling a Flapping Wing MAV Flight Path Reconstruction of the Delfly II
- 2013Modeling a Flapping Wing MAV: Flight path reconstruction of the Delfly II
- 2013A joint sensor based backstepping approach for fault-tolerant flight control of a large civil aircraft
- 2013Multivariate simplex spline based nonlinear dynamic inversion control of high performance aircraft
- 2013A Hybrid Sensor Based Backstepping Control Approach with its Application to Fault-Tolerant Flight Controlcitations
- 2013Online Aerodynamic Model Identification using a Recursive Sequential Method for Multivariate Splinescitations
- 2011Global Nonlinear Model Identification with Multivariate Splines
- 2009Lyapunov-based fault tolerant flight control designs for a modern fighter aircraft model
Places of action
conferencepaper
Motion Simulator 2-Axis Input Design for Angular Accelerometer Calibration
Abstract
The calibration of Angular Accelerometers requires a controlled test with a known acceleration profile. However, current turn-tables have been designed primarily for generating a constant rotational velocity. To generate a profile with varying angular acceleration we propose using constant rotational velocity on the two axes of a 2-axes motion simulator. The proposed sequence was developed to obtain the required rotational acceleration signal quality using only rotational velocity input. The identified pattern is applied to an envelope of test conditions, resulting in test matrix. This method provides an alternative means to generate inputs that can be used to calibrate angular accelerometers using calibration hardware that is not primarily designed to provide accurate acceleration inputs.<br/>
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