| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A Box Regularized Particle Filter for terrain navigation with highly non-linear measurements * * The authors would like to thank the COGENT Computing lab (Coventry University) for their financial support.
|
Merlinge, Nicolas
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2016
|
49 |
17 |
p. 361-366
6 p.
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artikel
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| 2 |
Accurate Autonomous Landing of a Fixed-Wing Unmanned Aircraft under Crosswind Conditions
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de Bruin, Andrew
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2016
|
49 |
17 |
p. 170-175
6 p.
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artikel
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| 3 |
A Comparative Study of Three Differentiation Schemes for the Detection of Runaway Faults in Aircraft Control Surfaces
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Cieslak, J.
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2016
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49 |
17 |
p. 70-75
6 p.
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artikel
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| 4 |
Adaptive Backstepping Autopilot Design for Missiles of Fast Time-varying Velocity
|
Lee, Seokwon
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2016
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49 |
17 |
p. 474-479
6 p.
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artikel
|
| 5 |
Adaptive Control with Neural Networks-based Disturbance Observer for a Spherical UAV
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Matassini, Tommaso
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2016
|
49 |
17 |
p. 308-313
6 p.
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artikel
|
| 6 |
A Data-Driven Approach to Detect Faults in the Airbus Flight Control System
|
Goupil, Philippe
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2016
|
49 |
17 |
p. 52-57
6 p.
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artikel
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| 7 |
Aggressive Turn-Around Manoeuvres with an Agile Fixed-Wing UAV
|
Levin, Joshua M.
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2016
|
49 |
17 |
p. 242-247
6 p.
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artikel
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| 8 |
A Holistic Vision-based Hazard Detection Framework for Asteroid Landings
|
Yan, Yunfeng
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2016
|
49 |
17 |
p. 218-223
6 p.
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artikel
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| 9 |
A Model-based diagnosis method for transient and multiple faults of AOCS thrusters
|
Pittet, C.
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2016
|
49 |
17 |
p. 82-87
6 p.
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artikel
|
| 10 |
Analytic Solution of Projectile Motion with Quadratic Drag and Unity Thrust
|
Han, Seungyeop
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2016
|
49 |
17 |
p. 40-45
6 p.
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artikel
|
| 11 |
An Eigenstructure Assignment Embedded Unknown Input Observe Approach for Actuator Fault Detection in Quadrotor Dynamics
|
Negash, Lebsework
|
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2016
|
49 |
17 |
p. 426-431
6 p.
|
artikel
|
| 12 |
An Error Model of a Complementary Filter for use in Bayesian Estimation - The CF-EKF Filter
|
Lustosa, Leandro R.
|
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2016
|
49 |
17 |
p. 444-449
6 p.
|
artikel
|
| 13 |
Angular Momentum Based Steering Approach for Control Moment Gyroscopes * * This work has been financially supported by the Space Agency of the German Aerospace Center (DLR, Deutsches Zentrum für Luft- und Raumfahrt e.V.) with means of the German Ministry of Economy and Technology under support number 50 RR 1302.
|
Geshnizjani, Ramin
|
|
2016
|
49 |
17 |
p. 141-145
5 p.
|
artikel
|
| 14 |
An Improved Dual-axis Mirror Control Scheme for Imaging LIDAR Application
|
Daning, Zhou
|
|
2016
|
49 |
17 |
p. 124-129
6 p.
|
artikel
|
| 15 |
An Innovation Approach Based Sensor Fault Detection and Isolation
|
Hajiyev, Chingiz
|
|
2016
|
49 |
17 |
p. 420-425
6 p.
|
artikel
|
| 16 |
Application of Input and State Multiple Model Adaptive Estimator for Aircraft Airspeed Approximation
|
Bauer, Péter
|
|
2016
|
49 |
17 |
p. 76-81
6 p.
|
artikel
|
| 17 |
Closed-loop actuator identification for Brazilian Thrust Vector Control development
|
Wekerle, Timo
|
|
2016
|
49 |
17 |
p. 468-473
6 p.
|
artikel
|
| 18 |
Close-Range 3D Collision Prediction under Attitude Uncertainty for On-Orbit Servicing Missions
|
Posch, A.
|
|
2016
|
49 |
17 |
p. 224-229
6 p.
|
artikel
|
| 19 |
Combined Geometric and Neural Network Approach to Generic Fault Diagnosis in Satellite Actuators and Sensors
|
Baldi, P.
|
|
2016
|
49 |
17 |
p. 432-437
6 p.
|
artikel
|
| 20 |
Combining sensor monitoring and fault tolerant control to maintain flight control system functionalities
|
Ossmann, D.
|
|
2016
|
49 |
17 |
p. 46-51
6 p.
|
artikel
|
| 21 |
Commercial Aircraft Lateral Flight Reference Trajectory Optimization
|
Murrieta-Mendoza, Alejandro
|
|
2016
|
49 |
17 |
p. 1-6
6 p.
|
artikel
|
| 22 |
Comparison of Aeroelastic Modeling and Robust Flutter Analysis of a Typical Section * * This work has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No 636307, project FLEXOP
|
Iannelli, A.
|
|
2016
|
49 |
17 |
p. 409-414
6 p.
|
artikel
|
| 23 |
Contents
|
|
|
2016
|
49 |
17 |
p. i-vi
nvt p.
|
artikel
|
| 24 |
Control of Magnetic Space Tug
|
Fabacher, Emilien
|
|
2016
|
49 |
17 |
p. 278-283
6 p.
|
artikel
|
| 25 |
Data-driven attitude control law of a variable-pitch quadrotor: a comparison study
|
Invernizzi, Davide
|
|
2016
|
49 |
17 |
p. 236-241
6 p.
|
artikel
|
| 26 |
Design and Development of a Novel Spherical UAV
|
Malandrakis, K.
|
|
2016
|
49 |
17 |
p. 320-325
6 p.
|
artikel
|
| 27 |
Discrete Sliding Mode control of small UAS in tight formation flight under information constraints
|
Bolting, Jan
|
|
2016
|
49 |
17 |
p. 332-337
6 p.
|
artikel
|
| 28 |
Embedded Model Control for UAV Quadrotor via Feedback Linearization
|
Lotufo, M.A.
|
|
2016
|
49 |
17 |
p. 266-271
6 p.
|
artikel
|
| 29 |
Evaluation of Guidance and Control System of D–SEND#2
|
Ninomiya, Tetsujiro
|
|
2016
|
49 |
17 |
p. 106-111
6 p.
|
artikel
|
| 30 |
Experimental Verification of Attitude Control System for Agile Spacecraft
|
Kornienko, Andrei
|
|
2016
|
49 |
17 |
p. 158-163
6 p.
|
artikel
|
| 31 |
Fast Marching Square Method for UAVs Mission Planning with consideration of Dubins Model Constraints
|
González, Verónica
|
|
2016
|
49 |
17 |
p. 164-169
6 p.
|
artikel
|
| 32 |
Fast Nonsingular Terminal Sliding Mode to Attenuate the Chattering for Missile Interception with Finite Time Convergence
|
Lyu, Shi
|
|
2016
|
49 |
17 |
p. 34-39
6 p.
|
artikel
|
| 33 |
Fault-Tolerant Control of a Boeing 747-100/200 Based on a Laguerre Function-Based MPC Scheme
|
Yu, Bin
|
|
2016
|
49 |
17 |
p. 58-63
6 p.
|
artikel
|
| 34 |
Fault-Tolerant Low-Thrust Trajectory Design with Backups for Multiple Targets
|
Wachi, Akifumi
|
|
2016
|
49 |
17 |
p. 391-396
6 p.
|
artikel
|
| 35 |
Flight Control Software Failure Mitigation: Design Optimization for Software-implemented Fault Detectors
|
Morozov, Andrey
|
|
2016
|
49 |
17 |
p. 248-253
6 p.
|
artikel
|
| 36 |
Gain-Scheduled Model-Matching Flight Controller Using Inexact Scheduling Parameters * * Supported by JSPS KAKENHI Grant 15K06159
|
Sato, Masayuki
|
|
2016
|
49 |
17 |
p. 88-93
6 p.
|
artikel
|
| 37 |
Geometrical Vertical Trajectory Optimization – Comparative Performance Evaluation of Phase versus Phase and Altitude-Dependent Preferred Gradient Selection
|
Dancila, Bogdan Dumitru
|
|
2016
|
49 |
17 |
p. 17-22
6 p.
|
artikel
|
| 38 |
Guidance, Navigation, and Control for Docking of Two Cubic Blimps
|
Abouzakhm, Patrick
|
|
2016
|
49 |
17 |
p. 260-265
6 p.
|
artikel
|
| 39 |
Hidden Coupling Terms Inclusion in Gain-Scheduling Control Design: Extension of an Eigenstructure Assignment-Based Technique * * This work was supported by NSERC under Grant RGPIN-2014-03942 and RGPIN-312116-13.
|
Lhachemi, H.
|
|
2016
|
49 |
17 |
p. 403-408
6 p.
|
artikel
|
| 40 |
HJB approach for a multi-boost launcher trajectory optimization problem * * This work is partially supported by Centre National d’Etudes Spa-tiales (CNES), under the grant RT-CR-430-1304-CNES, by iCODE Institute project funded by the IDEX Paris-Saclay, ANR-11-IDEX-0003-02, and by DGA under the grant DGA-ENSTA-06-60-037
|
Bokanowsky, Olivier
|
|
2016
|
49 |
17 |
p. 456-461
6 p.
|
artikel
|
| 41 |
H ∞ Structured Controller Synthesis Applied to Flight Controller of QTW-UAV Using Meta-Heuristic Particle Swarm Optimization
|
Nami, Chiramathe
|
|
2016
|
49 |
17 |
p. 326-331
6 p.
|
artikel
|
| 42 |
Hybrid Impedance/Position Control of a Free-Flying Space Robot for Detumbling a Noncooperative Satellite
|
Uyama, N.
|
|
2016
|
49 |
17 |
p. 230-235
6 p.
|
artikel
|
| 43 |
Implementation of real-time moving horizon estimation for robust air data sensor fault diagnosis in the RECONFIGURE benchmark * * This work has received funding from the European Union’s Seventh Framework Programme (FP7-RECONFIGURE/2007-2013) under grant agreement no. 314544.
|
Wan, Yiming
|
|
2016
|
49 |
17 |
p. 64-69
6 p.
|
artikel
|
| 44 |
Integrated Control/Structure Design of a Large Space Structure using Structured H ∞ Control
|
Perez, J. Alvaro
|
|
2016
|
49 |
17 |
p. 302-307
6 p.
|
artikel
|
| 45 |
Linearized Impulsive Fixed-Time Fuel-Optimal Space rendezvous: A New Numerical Approach
|
Arzelier, Denis
|
|
2016
|
49 |
17 |
p. 373-378
6 p.
|
artikel
|
| 46 |
Linear Modeling of a Flexible Substructure Actuated through Piezoelectric Components for Use in Integrated Control/Structure Design
|
Perez, J. Alvaro
|
|
2016
|
49 |
17 |
p. 296-301
6 p.
|
artikel
|
| 47 |
LMI-based design of a robust direct adaptive attitude control for a satellite with uncertain parameters * * This research is supported by CNES Centre National d’Etudes Spatiales and région Midi-Pyrénées
|
Leduc, Harmonie
|
|
2016
|
49 |
17 |
p. 367-372
6 p.
|
artikel
|
| 48 |
Longitudinal System Identification of Ornithopter with Automated Flight Tests * * This research was supported by a grant to Bio-Mimetic Robot Research Center funded by Defense Acquisition Program Administration (UD130070ID).
|
Gim, Hakseong
|
|
2016
|
49 |
17 |
p. 194-199
6 p.
|
artikel
|
| 49 |
LPV Control and Singularity Avoidance of a Spacecraft with DGCMGs
|
Sasaki, Takahiro
|
|
2016
|
49 |
17 |
p. 152-157
6 p.
|
artikel
|
| 50 |
Measurement Differencing Approach Based Kalman Filter Applied To INS Error Compensation
|
Hajiyev, Chingiz
|
|
2016
|
49 |
17 |
p. 343-348
6 p.
|
artikel
|
| 51 |
Modelling, Simulation and Flight Test of a Model Predictive Controlled Multirotor with Heavy Slung Load
|
Notter, S.
|
|
2016
|
49 |
17 |
p. 182-187
6 p.
|
artikel
|
| 52 |
Nonlinear Dynamic Inversion of a Flexible Aircraft
|
Caverly, Ryan James
|
|
2016
|
49 |
17 |
p. 338-342
5 p.
|
artikel
|
| 53 |
Nonlinear projection filter for target tracking using range sensor & optical tracker * * This research is supported by EPSRC Research Grant, EP/N010523/1, Balancing the impact of city infrastructure engineering on natural systems using robots.
|
Kim, Jongrae
|
|
2016
|
49 |
17 |
p. 438-443
6 p.
|
artikel
|
| 54 |
Optimal Control for Minimum-Fuel Geostationary Station Keeping of Satellites Equipped with Electric Propulsion
|
Gazzino, C.
|
|
2016
|
49 |
17 |
p. 379-384
6 p.
|
artikel
|
| 55 |
Optimal Control of Payload Tossing Using Space Tethered System
|
Shi, Lu Hong
|
|
2016
|
49 |
17 |
p. 272-277
6 p.
|
artikel
|
| 56 |
Optimal-Switched H ∞ Robust Tracking for Maneuvering Space Target
|
Li, Yuankai
|
|
2016
|
49 |
17 |
p. 415-419
5 p.
|
artikel
|
| 57 |
Optimal Threshold Policy for Sequential Weapon Target Assignment
|
Kalyanam, Krishnamoorthy
|
|
2016
|
49 |
17 |
p. 7-10
4 p.
|
artikel
|
| 58 |
Orbit and Formation Control for the Next Generation Gravity Mission * * Part of this research was carried out within the study Next Generation Gravity Mission (NGGM): AOCS Solutions and Technologies study and within the ESA Networking Partner Initiative (NPI) PhD project Laser Metrology Spacecraft Formation (Ref. 4000109653/13/NL/MH) funded by the European Space Agency; Thales Alenia Space Italy (Turin) being the prime contractor
|
Colangelo, L.
|
|
2016
|
49 |
17 |
p. 284-289
6 p.
|
artikel
|
| 59 |
Performance Assessment of a Gyroless 3-Axis Stabilised Sun Pointing Mode on a Highly Elliptical Orbit
|
Woo, Pamela
|
|
2016
|
49 |
17 |
p. 146-151
6 p.
|
artikel
|
| 60 |
Preparation of Papers for IFAC Conferences & Symposia: Guidance, Navigation, and Control for Future Miniature Satellite Formations: Current Limitations and Impending Advancements
|
Bangert, Philip
|
|
2016
|
49 |
17 |
p. 290-295
6 p.
|
artikel
|
| 61 |
Preview Feedforward Compensation: LMI Synthesis and Flight Simulation
|
Hamada, Yoshiro
|
|
2016
|
49 |
17 |
p. 397-402
6 p.
|
artikel
|
| 62 |
PSO-based Optimal Task Allocation for Cooperative Timing Missions
|
Oh, Gyeongtaek
|
|
2016
|
49 |
17 |
p. 314-319
6 p.
|
artikel
|
| 63 |
Quadrotor UAV state estimation based on High-Degree Cubature Kalman filter
|
Benzerrouk, Hamza
|
|
2016
|
49 |
17 |
p. 349-354
6 p.
|
artikel
|
| 64 |
Reaction Sphere Actuator * * This work was supported by projects "Project FCT PEst-OE/EEI/LA0009/2013" and "GMVAD MVFLAU/IST 31575/13".
|
Craveiro, António Amaral
|
|
2016
|
49 |
17 |
p. 212-217
6 p.
|
artikel
|
| 65 |
Real time Autopilot based on Immersion & Invariance for Autonomous Aerial Vehicle
|
Bouzid, Y.
|
|
2016
|
49 |
17 |
p. 176-181
6 p.
|
artikel
|
| 66 |
Relative Motion Control of PicoSatellites Constellation in Independent Orbits
|
Nebylov, A.V.
|
|
2016
|
49 |
17 |
p. 355-360
6 p.
|
artikel
|
| 67 |
Reusable Space Planes Challenges And Control Problems
|
Nebylov, Alexander
|
|
2016
|
49 |
17 |
p. 480-485
6 p.
|
artikel
|
| 68 |
Robust Capture Zone Approximation by Interval Integration with Uncertainty
|
Turetsky, Vladimir
|
|
2016
|
49 |
17 |
p. 28-33
6 p.
|
artikel
|
| 69 |
Robustness Assessment of a Load Factor Flight Control Law Using Dilation Integrals * * This work was supported by NSERC under Grant RGPIN-2014-03942 and RGPIN-2012-122106.
|
Bessadi, K.
|
|
2016
|
49 |
17 |
p. 94-99
6 p.
|
artikel
|
| 70 |
Robust Supervisory Control of a Spacecraft Propulsion System
|
Yari, Farid
|
|
2016
|
49 |
17 |
p. 200-205
6 p.
|
artikel
|
| 71 |
Sensitivity Analysis on Weight and Trajectory Optimization Results for Multistage Guided Missile
|
Hong, Seong-Min
|
|
2016
|
49 |
17 |
p. 23-27
5 p.
|
artikel
|
| 72 |
Slack Variables Generation via QR Decomposition for Adaptive Nonlinear Control of Affine Underactuated Systems
|
Kim, Mingu
|
|
2016
|
49 |
17 |
p. 188-193
6 p.
|
artikel
|
| 73 |
Structured H∞ synthesis for flexible launcher control
|
Ganet-Schoeller, M.
|
|
2016
|
49 |
17 |
p. 450-455
6 p.
|
artikel
|
| 74 |
Technology for determining the local vertical of nanosatellite by processing videoimages of the Earth horizon
|
Lomaka, Igor
|
|
2016
|
49 |
17 |
p. 206-211
6 p.
|
artikel
|
| 75 |
Three-Axis Attitude Maneuver of Spacecraft by Reaction Wheels with Rotation Speed Constraints
|
Nomura, Shunichiro
|
|
2016
|
49 |
17 |
p. 130-134
5 p.
|
artikel
|
| 76 |
Tilt-rotor multivariable attitude control with rotor state feedback
|
Panza, S.
|
|
2016
|
49 |
17 |
p. 100-105
6 p.
|
artikel
|
| 77 |
Trajectory Optimization for vertical navigation using the Harmony Search algorithm
|
Ruby, Margaux
|
|
2016
|
49 |
17 |
p. 11-16
6 p.
|
artikel
|
| 78 |
Trajectory Planning for Terminal Area Energy Management Phase of Reusable Launch Vehicles
|
Mu, Lingxia
|
|
2016
|
49 |
17 |
p. 462-467
6 p.
|
artikel
|
| 79 |
Two-Level Nonlinear Tracking Control of a Quadrotor Unmanned Aerial Vehicle
|
KÖKSAL, Nasrettin
|
|
2016
|
49 |
17 |
p. 254-259
6 p.
|
artikel
|
| 80 |
V-bar and R-bar Glideslope Guidance Algorithms for Fixed-Time Rendezvous: A Linear Programming Approach
|
Ariba, Yassine
|
|
2016
|
49 |
17 |
p. 385-390
6 p.
|
artikel
|
| 81 |
Vision-based control for helicopter ship landing with handling qualities constraints
|
Truong, Quang Huy
|
|
2016
|
49 |
17 |
p. 118-123
6 p.
|
artikel
|
| 82 |
Visual-Aided INS Using Converted Measurements
|
Montgomery, Turner J.
|
|
2016
|
49 |
17 |
p. 112-117
6 p.
|
artikel
|
| 83 |
Zero-Speed Crossing Avoidance with Three Active Reaction Wheels using Set-Point Angular Momentum Management
|
Sampaio, Ulisses P.
|
|
2016
|
49 |
17 |
p. 135-140
6 p.
|
artikel
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