| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A computationally efficient model predictive control scheme for space debris rendezvous
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Larsén, Alexander Korsfeldt
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52 |
12 |
p. 103-110
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artikel
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| 2 |
Active Fault-tolerant Gyromoment Control of Satellites and Free-flying Robots
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Rodnishchev, N.
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52 |
12 |
p. 182-187
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artikel
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| 3 |
Active flutter suppression: non-structured and structured H ∞ design * ⁎ This project has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No 636307.
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Waitman, Sérgio
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52 |
12 |
p. 146-151
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artikel
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| 4 |
Active Sampling-based Data-driven Reachability Verification for Proportional Navigation Guidance Law
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Lee, Suwon
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52 |
12 |
p. 1-6
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artikel
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| 5 |
Adaptive Control of Novel Configuration with Moving Mass
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Li, Jianqing
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52 |
12 |
p. 508-513
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artikel
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| 6 |
Addressing Actuation Redundancies in Incremental Controllers for Attitude Tracking of Fixed-Wing Aircraft * ⁎ This research is co-funded by the European Union in the scope of INCEPTION project, which has received funding from the EU Horizon 2020 Research and Innovation Programme under grant agreement No. 723515, and by FCT, through IDMEC, under LAETA, project UID/EMS/50022/2019.
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Cordeiro, Rafael A.
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52 |
12 |
p. 417-422
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artikel
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| 7 |
A design of a short course with COTS UAV system for higher education students
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Hong, Ju-Hyeon
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52 |
12 |
p. 466-471
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artikel
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| 8 |
A Kalman Filtering Approach for Systems Subject to Parametric Modeling Uncertainties
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Stoica, Adrian M.
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52 |
12 |
p. 400-404
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artikel
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| 9 |
A Method for Misalignment Correction of Star Sensors
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Strietzel, Roland
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52 |
12 |
p. 43-48
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artikel
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| 10 |
An Event-Triggered Predictive Controller for Spacecraft Rendezvous Hovering Phases
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Sanchez, Julio C.
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52 |
12 |
p. 97-102
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artikel
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| 11 |
A new control allocation algorithm to improve runway centerline tracking at landing
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Sadien, Edouard
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52 |
12 |
p. 520-525
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artikel
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| 12 |
An Experience of Project Based Learning in Aerospace Engineering
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Castaldi, Paolo
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52 |
12 |
p. 484-489
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artikel
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| 13 |
An MPC Approach to Transient Control of Liquid-Propellant Rocket Engines
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Pérez-Roca, Sergio
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52 |
12 |
p. 268-273
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artikel
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| 14 |
Application of LQG and H∞ Gain Scheduling Techniques to Active Suppression of Flutter
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Rosique, Miguel Á
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52 |
12 |
p. 502-507
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artikel
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| 15 |
Area Coverage by a Group of UAVs using the Broadcast Control Framework
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Darmaraju, Shalini
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52 |
12 |
p. 370-375
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artikel
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| 16 |
Ascent Trajectory Optimization of Launch Vehicles with Air-Breathing Propulsion
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Mukundan, Vijith
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52 |
12 |
p. 274-279
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artikel
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| 17 |
A Super-Twisting Sliding Mode Control in a Backstepping Setup for Rendezvous with a Passive Target * ⁎ This work is supported by CONACyT under grant 440473 (CVU 594664), by SIP-IPN under grant 20180865 and by CDA-IPN.
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Torres, Jazmín Zenteno
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52 |
12 |
p. 25-30
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artikel
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| 18 |
Attitude stabilization of inertial pointing spacecraft using magnetic actuators
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Invernizzi, Davide
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52 |
12 |
p. 442-447
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artikel
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| 19 |
Automatic Three-Point Landing of a UAV with H ∞-Control in D-Implementation
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Sedlmair, Nicolas
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52 |
12 |
p. 316-321
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artikel
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| 20 |
Closed-loop Analysis with Incremental Backstepping Controller considering Measurement Bias
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Jeon, Byoung-Ju
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52 |
12 |
p. 405-410
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artikel
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| 21 |
Co-design of aircraft vertical tail and control laws using distributed electric propulsion * ⁎ This work is supported by AIRBUS and ONERA.
|
Van, E. Nguyen
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52 |
12 |
p. 514-519
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artikel
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| 22 |
Collision-Free Decentralised Density Feedback Control for Swarms * ⁎ Authors have contributed equally to this work.
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Eren, Utku
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52 |
12 |
p. 364-369
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artikel
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| 23 |
Combining Homogeneous High Order Sliding Mode and Nonlinear Dynamic Inversion for fixed wing aircraft attitude and speed control
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Hamissi, A.
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52 |
12 |
p. 304-309
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artikel
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| 24 |
Computational Guidance Using Sparse Gauss-Hermite Quadrature Differential Dynamic Programming
|
He, Shaoming
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52 |
12 |
p. 13-18
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artikel
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| 25 |
Contents
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52 |
12 |
p. i-vii
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artikel
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| 26 |
Control Technologies and Instrumentation in Aerospace Engineering
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Nebylov, Alexander V.
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52 |
12 |
p. 472-477
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artikel
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| 27 |
Convertible delta-wing aircraft for teaching and research * ⁎ This paper has been supported by the French Agence Nationale de la Recherche (ANR), Projet MICA ANR-16-CE22-0003, and by the Centre de Ressources IMA (Univ. Bordeaux).
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Airimitoaie, Tudor-Bogdan
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52 |
12 |
p. 478-483
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artikel
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| 28 |
Cooperative guidance of a fleet of UAVs for multi-target discovery and tracking in presence of obstacles using a set membership approach * ⁎ This work has been performed with DGA support.
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Reboul, Léon
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52 |
12 |
p. 340-345
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artikel
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| 29 |
Cooperative State and Fault Estimation of Formation Flight of Satellites in Deep Space Subject to Unreliable Information
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Azizi, S.M.
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52 |
12 |
p. 206-213
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artikel
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| 30 |
Cryogenic Liquid Rocket Engine Test Bench Fault-Tolerant Control System: Cooling System Application
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Sarotte, C.
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52 |
12 |
p. 280-285
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artikel
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| 31 |
Deep Neural Network-Based Feedback Control for Dynamic Soaring of Unpowered Aircraft * ⁎ This work was supported by the R&D Program in Aerospace Parts and Materials (10066055) through the Korea Evaluation Institute of Industrial Technology funded by the Ministry of Trade, Industry, and Energy, Republic of Korea.
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Kim, Seong-hun
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52 |
12 |
p. 117-121
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artikel
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| 32 |
Digital and Pulse-width Control of the Satellites and Space Robots Orientation in Initial Modes
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Somov, Ye.
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52 |
12 |
p. 544-548
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artikel
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| 33 |
3D UAV Navigation with Moving-Obstacle Avoidance Using Barrier Lyapunov Functions
|
Restrepo, Esteban
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52 |
12 |
p. 49-54
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artikel
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| 34 |
Energy Management and Guidance for Gyroplane Autonomous Unpowered Landing Based on Onboard Trajectory Generation
|
Fang, Xiaoxing
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52 |
12 |
p. 250-255
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artikel
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| 35 |
Ensuring of Relative Navigation and Control of Low-Orbital Microsatellites Formation in the Task of Remote Control of Robots
|
Nebylov, Alexander V.
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52 |
12 |
p. 238-243
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artikel
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| 36 |
Evolutionary Game Theory based Multi-Objective Optimization for Control Allocation of Over-Actuated System
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Park, On
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52 |
12 |
p. 310-315
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artikel
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| 37 |
Experimental validation of LMI-based anti-windup compensators for attitude control in multirotor UAVs
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Buratti, Nicolò
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52 |
12 |
p. 164-169
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artikel
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| 38 |
Fast Trajectory Optimization using Sequential Convex Programming with No-Fly Zone Constraints
|
Oh, Young-Jae
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52 |
12 |
p. 298-303
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artikel
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| 39 |
Fault analysis to improve reliability of a LEO satellite EPS
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Mostacciuolo, E.
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52 |
12 |
p. 200-205
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artikel
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| 40 |
Finite Horizon Worst Case Analysis of Launch Vehicles * ⁎ This work is partially funded by ESA through the Networking/Partnering Initiative contract No. 540-2017.
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Biertümpfel, Felix
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52 |
12 |
p. 31-36
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artikel
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| 41 |
Finite-time Attitude Tracking Control Method of Microsatellite Based on Adaptive Robustness and Neural Network Approximation
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Kaicheng, Zhang
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52 |
12 |
p. 85-90
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artikel
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| 42 |
Guidance and Control of a Space Robot-manipulator at Approach and Capturing a Passive Satellite* ⁎ The work was supported by the RFBR, Grant no. 17-08-01708.
|
Somov, Ye.
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52 |
12 |
p. 538-543
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artikel
|
| 43 |
Gust Alleviation Control using Prior Gust Information: Wind Tunnel Test Results
|
Hamada, Yoshiro
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52 |
12 |
p. 128-133
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artikel
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| 44 |
Hierarchical Model Predictive Control for Autonomous Vehicle Area Coverage
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Ibrahim, M.
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52 |
12 |
p. 79-84
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artikel
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| 45 |
Hierarchic Stabilization of Flying Convex-Path-Following Formations Part I: Fully-Actuated Agents
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El-Hawwary, Mohamed I.
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52 |
12 |
p. 346-351
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artikel
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| 46 |
Hierarchic Stabilization of Flying Convex-Path-Following Formations Part II: Underactuated Agents
|
El-Hawwary, Mohamed I.
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52 |
12 |
p. 352-357
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artikel
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| 47 |
H∞/LQR Optimal Control for a Supersonic Air-Breathing Missile of Asymmetric Configuration * ⁎ This project is part-sponsored by the Defence Science and Technology Laboratory (DSTL) of the United Kingdom and the other part by Cranfield University.
|
Vincent, Raymond Vin
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52 |
12 |
p. 214-218
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artikel
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| 48 |
Improved IMC-Filter Design to IMC-PI Equivalence: Application to Quadrotor
|
Bouzid, Y.
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52 |
12 |
p. 158-163
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artikel
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| 49 |
Integration of Phase Plane Flight Envelope Protections in Cascaded Incremental Flight Control * ⁎ This research is co-funded by the European Union in the scope of INCEPTION project, which has received funding from the EU’s Horizon2020 Research and Innovation Programme under grant agreement No. 723515.
|
Gabrys, Agnes Christine
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52 |
12 |
p. 429-435
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artikel
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| 50 |
Inverse Dynamics based Model Predictive Control for Spacecraft Rapid Attitude Maneuver
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Song, Chao
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52 |
12 |
p. 111-116
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artikel
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| 51 |
LEO satellites Based Doppler Positioning Using Distributed nonlinear Estimation
|
Benzerrouk, Hamza
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52 |
12 |
p. 496-501
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artikel
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| 52 |
Linear Quadratic Regulator for Trajectory Tracking of a Quadrotor
|
Martins, Luís
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52 |
12 |
p. 176-181
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artikel
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| 53 |
Missile Initial Engagement Determination and Terminal Phase Guidance
|
Fariz, A.
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52 |
12 |
p. 19-24
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artikel
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| 54 |
MMAE/LQR Yaw Control System of a Quadrotor for Constant Unknown Inertia * ⁎ This work was supported by FCT, through IDMEC, under LAETA, project UID/EMS/50022/2019 and project LOTUS of FCT - PTDC/EEI-AUT/5048/2014.
|
Outeiro, Pedro
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52 |
12 |
p. 170-175
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artikel
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| 55 |
Model-based Dependability Analysis of Fault-tolerant Inertial Navigation System: A Practical Experience Report
|
Steurer, Mikael
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52 |
12 |
p. 394-399
|
artikel
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| 56 |
Model Based Driving Analysis for A novel Stepped Rotary Flow Control Valve * ⁎ Acknowledgment for the industrial cooperation by HYDRECO Hydraulics ltd
|
Abuowda, Karem
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52 |
12 |
p. 549-554
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artikel
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| 57 |
Model-based FDI for Agile Spacecraft with Multiple Actuators Working Simultaneously
|
Lopez-Encarnacion, E.
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52 |
12 |
p. 436-441
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artikel
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| 58 |
Multi-vehicle Cooperative Control for Load Transportation * ⁎ This work was partially supported by the projects MYRG2018-00198-FST of the University of Macau; by the Macau Science and Technology, Development Fund under Grant FDCT/026/2017/A1 by Fundao para a Cincia e a Tecnologia (FCT) through the projects UID/EEA/50009/2019, LOTUS - PTDC/EEIAUT/ 5048/2014, HARMONY - PTDC/EEI-AUT/31411/2017.
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Valentim, Tiago
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52 |
12 |
p. 358-363
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artikel
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| 59 |
New technique for deploying long coilable booms, without blossoming effect, using a polymer joint
|
Cornogolub, A.
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52 |
12 |
p. 555-559
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artikel
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| 60 |
Nonlinear Robust Generalized Dynamic Inversion based Homing Guidance and Control of Aerial Interceptors
|
Ansari, Uzair
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52 |
12 |
p. 219-226
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artikel
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| 61 |
Novel Non-Model-Based Fault Detection and Isolation of Satellite Reaction Wheels Based on a Mixed-Learning Fusion Framework
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Nozari, Hasan Abbasi
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52 |
12 |
p. 194-199
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artikel
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| 62 |
Optimal guidance for 1st stage launcher recovery
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Ganet-Schoeller, Martine
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52 |
12 |
p. 532-537
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artikel
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| 63 |
Optimization of the control system for collecting a group of vehicles
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Panferov, Aleksandr I.
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52 |
12 |
p. 244-249
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artikel
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| 64 |
Performance Analysis of Modified Gain Pseudo-Measurement Filter for Ballistic Target Tracking
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Lee, Dong-Yeon
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52 |
12 |
p. 7-12
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artikel
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| 65 |
Performance Evaluation of Learning-Based Channel Prediction for Communication Relay UAVs in Urban Environments * ⁎ This work was supported by the Basic Science Research Program through the Lockheed Martin Corporation Republic of Korea Science, Technology, Research (RoKST&R) Initiative and the National Research Foundation of Korea (NRF) funded by the Ministry of Education (2017R1D1A1B03029992).
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Ladosz, Pawel
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52 |
12 |
p. 292-297
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artikel
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| 66 |
Position, Size and Orientation Estimation of Ground Obstacles in Sense and Avoid * ⁎ This paper was supported by the Janos Bolyai Research Scholarship of the Hungarian Academy of Sciences. The research presented in this paper was funded by the Higher Education Institutional Excellence Program. The research leading to these results has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No. 690811 and the Japan New Energy and Industrial Technology Development Organization under grant agreement No. 062600 as a part of the EU/Japan joint research project entitled ‘Validation of Integrated Safety-enhanced Intelligent flight cONtrol (VISION)’.
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Bauer, Peter
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52 |
12 |
p. 328-333
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artikel
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| 67 |
Preparation of Papers for IFAC Conferences & Symposia: Autonomous Distribution Algorithm for Formation Satellites Under Emergent Imaging Requests
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Yue, A. Miao
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52 |
12 |
p. 460-465
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artikel
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| 68 |
Propellant Sloshing Torque H ∞ – based Observer Design for Enhanced Attitude Control* ⁎ This study have been co-funded by ONERA and CNES
|
Bourdelle, Anthony
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52 |
12 |
p. 286-291
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artikel
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| 69 |
Quadrotor trajectory generation and tracking for aggressive maneuvers with attitude constraints
|
Yu, Gan
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52 |
12 |
p. 55-60
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artikel
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| 70 |
Reinforcement of a Reference Model-based Control using Active Disturbance Rejection principle: application to quadrotor
|
Bouzid, Y.
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52 |
12 |
p. 152-157
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artikel
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| 71 |
Reliable Control Optimization in Aerospace Engineering at Stochastic Stream of Faults * ⁎ The work was supported by the RFBR, Grant no. 17-08-01708.
|
Rodnishchev, N.
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52 |
12 |
p. 188-193
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artikel
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| 72 |
Research on Speed Oscillation of Ultra-Low Speed Turntable in Aerospace Due to Limited Resolution Encoder
|
Li, Lidong
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52 |
12 |
p. 322-327
|
artikel
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| 73 |
Robust C* Control Law Design Augmented with LIDAR-Based Gust Information
|
Takase, Ryoichi
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52 |
12 |
p. 122-127
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artikel
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| 74 |
Robust Control based on ADRC and DOBC for Small-Scale Helicopter
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Yu, Beomyeol
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52 |
12 |
p. 140-145
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artikel
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| 75 |
Robust Design for the Roll-Channel Autopilot of a Canard-Guided Dual-Spin Projectile
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Thai, Sovanna
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52 |
12 |
p. 232-237
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artikel
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| 76 |
Robust H ∞ Computed Torque Control of Flexible Joint TVC Systems
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Aydogan, A.
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52 |
12 |
p. 454-459
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artikel
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| 77 |
Runway Relative Positioning of Aircraft with IMU-Camera Data Fusion * ⁎ This paper was supported by the Janos Bolyai Research Scholarship of the Hungarian Academy of Sciences. The research presented in this paper was funded by the Higher Education Institutional Excellence Program. The research leading to these results has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No. 690811 and the Japan New Energy and Industrial Technology Development Organization under grant agreement No. 062600 as a part of the EU/Japan joint research project entitled ‘Validation of Integrated Safety-enhanced Intelligent flight control (VISION)’.
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Grof, Tamas
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52 |
12 |
p. 376-381
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artikel
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| 78 |
Scaling of commanded signals in a cascade control system addressing velocity and acceleration limitations of robotic UAVs
|
Łakomy, Krzysztof
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52 |
12 |
p. 73-78
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artikel
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| 79 |
SDRE Control with Nonlinear J2 Perturbations for Nanosatellite Formation Flying* ⁎ The authors thank all the collaborators of the Telematics Earth Observation Mission (TOM). TOM is supported by the Bavarian Ministry of Economic Affairs and Media, Energy and Technology
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Bilal, Mohd
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52 |
12 |
p. 448-453
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artikel
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| 80 |
Sense and Avoid using Hybrid Convolutional and Recurrent Neural Networks
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Navarro, Daniel Vidal
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52 |
12 |
p. 61-66
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artikel
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| 81 |
Shaft Speed Control of Laboratory Gas Turbine Engine
|
Singh, Richa
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52 |
12 |
p. 262-267
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artikel
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| 82 |
Space Micro-launcher H ∞ Control Under Parametric Modeling Uncertainties * ⁎ The authors acknowledge the financial support from the European Space Agency through contract number 4000119953/17/F/JLVs, Advanced Control Techniques for Future Launchers.
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Diaconescu, Sabin
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52 |
12 |
p. 91-96
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artikel
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| 83 |
Stage Optimization of Anti-Air Missiles Considering Guidance Laws
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Hong, Seong-Min
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52 |
12 |
p. 227-231
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artikel
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| 84 |
Stochastic Optimal Control for Collision Avoidance and Landing
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Shimizu, Yuji
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52 |
12 |
p. 37-42
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artikel
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| 85 |
System Identification and Feedforward Control of a Fatigue Structural Testing Rig: The Single Actuator Case * ⁎ This research was completed with support from the National Research Council of Canada.
|
Fortune, Robyn
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52 |
12 |
p. 382-387
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artikel
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| 86 |
Tensor Product Model-based Robust Flutter Control Design for the FLEXOP Aircraft
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Takarics, Béla
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52 |
12 |
p. 134-139
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artikel
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| 87 |
The WIG-craft Aerodynamic Model Parameters Calculation
|
Brodsky, Sergey A.
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52 |
12 |
p. 256-261
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artikel
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| 88 |
Towards Resilient UAV: Escape Time in GPS Denied Environment with Sensor Drift * ⁎ This work has been supported by the National Science Foundation (ECCS-1739732 and CMMI-1663460).
|
Yoon, Hyung-Jin
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52 |
12 |
p. 423-428
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artikel
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| 89 |
Trajectory planning and control for drone replacement for multidrone cinematography
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Marques, Marta
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52 |
12 |
p. 334-339
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artikel
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| 90 |
Trajectory Planning of the Unmanned Aerial Vehicles with Adaptive Convex Optimization Method * ⁎ This work was supported in part by the National Natural Science Foundation of China under Grants 61573061.
|
Sun, Xin
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52 |
12 |
p. 67-72
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artikel
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| 91 |
Two-Layer On-line Parameter Estimation for Adaptive Incremental Backstepping Flight Control for a Transport Aircraft in Uncertain Conditions
|
Ignatyev, Dmitry I.
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52 |
12 |
p. 411-416
|
artikel
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| 92 |
UAV Lab: a multidisciplinary UAV design course
|
Giurato, Mattia
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52 |
12 |
p. 490-495
|
artikel
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| 93 |
Validation of Control Laws at High Angles of Attack Using Three-Degree-of-Freedom Dynamic Rig in Wind Tunnel
|
Sidoryuk, Maria E.
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52 |
12 |
p. 526-531
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artikel
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| 94 |
Vision-Aided Complementary Filter for Attitude and Position Estimation: Design, Analysis and Experimental Validation
|
Madeiras, João
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52 |
12 |
p. 388-393
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artikel
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