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
Modelling an angular accelerometer using frequency-response measurements
Abstract
A characterization of an angular accelerometer sensor is performed with a frequency- response experiment. To assess angular accelerometer dynamic properties, a position-based calibration table is utilized to provide the excitation input. The angular accelerometer specifications and calibration table limitations dfine a constrained test envelope for this particular setup. Measurement are obtained for a number of constant accelerations and varied with frequency. Analysis of the input-output relation in the frequency-domain leads to a frequency-response function model of the angular accelerometer. Time-domain data are used to validate the frequency-response model. A fourth-order structure is then preferred as the transfer-function for the 400 deg=s acceleration, with a 99:02 %fit. Besides representing the angular accelerometer dynamics, the angular accelerometer model is es- sential for the design of fault-tolerant light control system.
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