| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active Fault Tolerant Control System for a High Accuracy Planet—Image and Stellar—Pointing Satellite
|
Bertoni, G.
|
|
2010
|
43 |
15 |
p. 422-427
6 p.
|
artikel
|
| 2 |
Active Formation Along an Eccentric Orbit
|
Bando, Mai
|
|
2010
|
43 |
15 |
p. 362-367
6 p.
|
artikel
|
| 3 |
Advanced Descent Scheme for Lunar Landing
|
Mehedi, Ibrahim M.
|
|
2010
|
43 |
15 |
p. 166-171
6 p.
|
artikel
|
| 4 |
An analysis of dissipation functions in swarming systems
|
Bennet, Derek J.
|
|
2010
|
43 |
15 |
p. 374-379
6 p.
|
artikel
|
| 5 |
Application of a Fault Accommodation Approach to a Re-***entry Vehicle
|
Marcos, Andrés
|
|
2010
|
43 |
15 |
p. 428-433
6 p.
|
artikel
|
| 6 |
Application of the Electrostatic Accelerometer MAC04 in Space Missions
|
Fedosov, Victor
|
|
2010
|
43 |
15 |
p. 517-522
6 p.
|
artikel
|
| 7 |
A solution for management of fault diagnosis and fault tolerance performances in active FTC schemes
|
Cieslak, J.
|
|
2010
|
43 |
15 |
p. 410-415
6 p.
|
artikel
|
| 8 |
A Study on the Dynamic Inversion with Lyapunov method
|
Enomoto, Keisuke
|
|
2010
|
43 |
15 |
p. 542-547
6 p.
|
artikel
|
| 9 |
A Suboptimal Guidance Design using Continuous-time MPSP with Input Inequality Constraint in a Hypersonic Mission
|
Maity, Arnab
|
|
2010
|
43 |
15 |
p. 160-165
6 p.
|
artikel
|
| 10 |
Attitude determination and control system for the Nano-JASMINE mission
|
Inamori, Takaya
|
|
2010
|
43 |
15 |
p. 253-258
6 p.
|
artikel
|
| 11 |
Automatic guidance of an aircraft using predictive control in a visual servoing scheme
|
Lumbar, Satja
|
|
2010
|
43 |
15 |
p. 1-6
6 p.
|
artikel
|
| 12 |
Closed Loop Stability of Synthetic Waypoint Guidance Algorithm
|
Medagoda, Eran D.B.
|
|
2010
|
43 |
15 |
p. 75-80
6 p.
|
artikel
|
| 13 |
Convergence and Optimality of Control Law for Periodic Maneuvering Satellites with CMGs
|
Ohmura, Takuya
|
|
2010
|
43 |
15 |
p. 548-553
6 p.
|
artikel
|
| 14 |
Cooperative Guidance for Naval Area Defence
|
Shin, Hyo-Sang
|
|
2010
|
43 |
15 |
p. 124-129
6 p.
|
artikel
|
| 15 |
Design of a Model-Following PID Control System for an MAV
|
Kondo, Hiroyuki
|
|
2010
|
43 |
15 |
p. 13-18
6 p.
|
artikel
|
| 16 |
Development and Operation of Microsatellite “MAIDO-1” and On-orbit Demonstration of Fudai Sun Sensor
|
Okubo, Hiroshi
|
|
2010
|
43 |
15 |
p. 247-252
6 p.
|
artikel
|
| 17 |
Dynamic Analysis and Adaptive Parameter Estimation for Variable Speed Control Moment Gyros with Uncertainty
|
JIN, Jin
|
|
2010
|
43 |
15 |
p. 484-489
6 p.
|
artikel
|
| 18 |
EKF-SLAM based Approach for Spacecraft Rendezvous Navigation with Unknown Target Spacecraft
|
Sonnenburg, Arne
|
|
2010
|
43 |
15 |
p. 339-344
6 p.
|
artikel
|
| 19 |
Enhanced Frameworks for Safety Verification of Autonomous Rendezvous Systems
|
Maier, Christoph
|
|
2010
|
43 |
15 |
p. 333-338
6 p.
|
artikel
|
| 20 |
Extended Model Recovery Anti-windup for Satellite Control 1
|
Boada, Josep
|
|
2010
|
43 |
15 |
p. 205-210
6 p.
|
artikel
|
| 21 |
Fault Detection and Isolation of an Aircraft Using Set-Valued Observers *
|
Rosa, Paulo
|
|
2010
|
43 |
15 |
p. 398-403
6 p.
|
artikel
|
| 22 |
Fault-Tolerant Control using a Virtual Actuator using LPV Techniques: Application to a Two-Degree of Freedom Helicopter
|
Oca, Saúl Montes de
|
|
2010
|
43 |
15 |
p. 416-421
6 p.
|
artikel
|
| 23 |
Flight-Formation Control of Air Vehicles Based on Collective Motion Control of Organisms
|
Inada, Yoshinobu
|
|
2010
|
43 |
15 |
p. 386-391
6 p.
|
artikel
|
| 24 |
Flight Vehicle System Identification via Nonlinear Smoothing Combined with Unscented Transform
|
Yokoyama, Nobuhiro
|
|
2010
|
43 |
15 |
p. 458-463
6 p.
|
artikel
|
| 25 |
FUZZY LOGIC BASED AUTONOMOUS LANDING SYSTEM FOR UNMANNED AERIAL VEHICLES
|
Kaynak, Okyay
|
|
2010
|
43 |
15 |
p. 63-70
8 p.
|
artikel
|
| 26 |
GNC technologies for NEO missions
|
Cavel, C.
|
|
2010
|
43 |
15 |
p. 271-276
6 p.
|
artikel
|
| 27 |
Gravity-Coulomb Force Combined Three-Body Problem
|
Yamakawa, Hiroshi
|
|
2010
|
43 |
15 |
p. 350-354
5 p.
|
artikel
|
| 28 |
Guidance and Control for Chase UAV via Sliding Mode Approach
|
Yamasaki, Takeshi
|
|
2010
|
43 |
15 |
p. 57-62
6 p.
|
artikel
|
| 29 |
Guidance and Robust Gyromoment Attitude Control of Agile Observation Satellite *
|
Somov, Ye. I.
|
|
2010
|
43 |
15 |
p. 218-223
6 p.
|
artikel
|
| 30 |
Guidance and Robust Pulse-width Control of an Information Satellite at Initial Modes *
|
Somov, Sergey
|
|
2010
|
43 |
15 |
p. 303-308
6 p.
|
artikel
|
| 31 |
Gust Alleviation Flight Controller Using Robust Model Predictive Control
|
Sato, Masayuki
|
|
2010
|
43 |
15 |
p. 7-12
6 p.
|
artikel
|
| 32 |
Identification and optimal control methodology for an active twist rotor
|
Rakotomamonjy, Thomas
|
|
2010
|
43 |
15 |
p. 452-457
6 p.
|
artikel
|
| 33 |
IMMUNE : Control reallocation after surface failures using model predictive control
|
Lafourcade, L.
|
|
2010
|
43 |
15 |
p. 446-451
6 p.
|
artikel
|
| 34 |
IMMUNE project : An overview
|
Döll, C.
|
|
2010
|
43 |
15 |
p. 434-439
6 p.
|
artikel
|
| 35 |
Impact Angle Constrained Suboptimal Terminal Guidance of Interceptors for Air Defence
|
Tatiya, Mayuri
|
|
2010
|
43 |
15 |
p. 130-135
6 p.
|
artikel
|
| 36 |
Impulsive Control of Satellite Formation Flying using Orbital Period Difference
|
Mok, Sunghoon
|
|
2010
|
43 |
15 |
p. 368-373
6 p.
|
artikel
|
| 37 |
In-flight Aircraft Monitoring using a Frequency Domain Parameter Identification
|
Hardier, G.
|
|
2010
|
43 |
15 |
p. 440-445
6 p.
|
artikel
|
| 38 |
Input-Shaped Link Motion for Attitude Control of Underactuated Planar Space Robot Equipped with Flexible Appendages
|
Kojima, Hirohisa
|
|
2010
|
43 |
15 |
p. 212-217
6 p.
|
artikel
|
| 39 |
INTEGRATED VALIDATION AND VERIFICATION FRAMEWORK FOR AUTONOMOUS RENDEZVOUS SYSTEMS
|
Di Sotto, Emanuele
|
|
2010
|
43 |
15 |
p. 315-320
6 p.
|
artikel
|
| 40 |
Intercept Guidance for Cooperative Aircraft Defense against a Guided Missile
|
Yamasaki, Takeshi
|
|
2010
|
43 |
15 |
p. 118-123
6 p.
|
artikel
|
| 41 |
Laser-based trajectory tracking H 2 control of autonomous rotorcraft
|
Guerreiro, B.J.
|
|
2010
|
43 |
15 |
p. 49-54
6 p.
|
artikel
|
| 42 |
Linear parameter-varying control of a large blended wing body flexible aircraft
|
Westermayer, C.
|
|
2010
|
43 |
15 |
p. 19-24
6 p.
|
artikel
|
| 43 |
Long-distance, drag-free, low-thrust, low-Earth-orbit formation control
|
Canuto, Enrico
|
|
2010
|
43 |
15 |
p. 297-302
6 p.
|
artikel
|
| 44 |
Mu-analysis Based Verification and Validation of Autonomous Satellite Rendezvous Systems
|
Kron, Aymeric
|
|
2010
|
43 |
15 |
p. 327-332
6 p.
|
artikel
|
| 45 |
Multiple Model Kalman Filter for Star Sensor Calibration
|
Kai, Xiong
|
|
2010
|
43 |
15 |
p. 471-476
6 p.
|
artikel
|
| 46 |
Multiple UAV Task Assignment using Descriptor Functions
|
Niccolini, Marta
|
|
2010
|
43 |
15 |
p. 93-98
6 p.
|
artikel
|
| 47 |
New Coning Error Compensation Method Using Direct Signal Estimation
|
Kang, Chul Woo
|
|
2010
|
43 |
15 |
p. 500-504
5 p.
|
artikel
|
| 48 |
New Star Identification Algorithm for Multiple Star Trackers with Unequal Qualities
|
Ho, Koki
|
|
2010
|
43 |
15 |
p. 477-482
6 p.
|
artikel
|
| 49 |
Nonlinear Optimal Reentry Guidance and Control of RLV in Pitch Plane
|
Halbe, O.
|
|
2010
|
43 |
15 |
p. 142-147
6 p.
|
artikel
|
| 50 |
Observability Analysis of Advanced Guidance Laws With Bearing-Only Measurement
|
Lee, Chang-Hun
|
|
2010
|
43 |
15 |
p. 136-141
6 p.
|
artikel
|
| 51 |
On GPS/GLONASS/INS Tight Integration for Gimbal and Strapdown Systems of Different Accuracy
|
Golovan, A.A.
|
|
2010
|
43 |
15 |
p. 505-509
5 p.
|
artikel
|
| 52 |
On-Orbit Experiment Results of Robust Symmetric Attitude Controller for ETS-VIII Spacecraft
|
Nagashio, Tomoyuki
|
|
2010
|
43 |
15 |
p. 199-204
6 p.
|
artikel
|
| 53 |
On the Definition of Curve's Frame at the Points of inflection
|
Shah, M. A
|
|
2010
|
43 |
15 |
p. 99-105
7 p.
|
artikel
|
| 54 |
Optimal Guidance Design for UAV Visual Target Tracking in an Urban Environment
|
Watanabe, Yoko
|
|
2010
|
43 |
15 |
p. 69-74
6 p.
|
artikel
|
| 55 |
Orbital Experiments of Linearly Interpolated Gain Scheduling Attitude Controller Using ETS-VIII Spacecraft
|
Hamada, Yoshiro
|
|
2010
|
43 |
15 |
p. 193-197
5 p.
|
artikel
|
| 56 |
Orbit estimation for a spacecraft by using Radiometric Observation
|
Ichikawa, Tsutomu
|
|
2010
|
43 |
15 |
p. 495-499
5 p.
|
artikel
|
| 57 |
Position control of a quad-rotor UAV using vision *
|
Carrillo, Luis Rodolfo Garcia
|
|
2010
|
43 |
15 |
p. 31-36
6 p.
|
artikel
|
| 58 |
Precise Landing of Space Probe on Asteroid Using Multiple Markers
|
Ogawa, Naoko
|
|
2010
|
43 |
15 |
p. 172-177
6 p.
|
artikel
|
| 59 |
Preliminary AOCS Design for Pointing Budget Assessment of the BIOMASS Candidate Earth Explorer Core Mission
|
Bennani,, Samir
|
|
2010
|
43 |
15 |
p. 309-314
6 p.
|
artikel
|
| 60 |
Principles and systems of heavy WIG-craft flight control
|
Nebylov, Alexander V.
|
|
2010
|
43 |
15 |
p. 106-111
6 p.
|
artikel
|
| 61 |
Prospective 3-Axis Attitude Control using Solar Radiation Pressure
|
Okano, Yoshinobu
|
|
2010
|
43 |
15 |
p. 229-233
5 p.
|
artikel
|
| 62 |
Quasi-LTV Polynomial Eigenstructure Assignment Control for Formation Flying Around Sun-Earth L2 Point *
|
Wang, Feng
|
|
2010
|
43 |
15 |
p. 345-350
6 p.
|
artikel
|
| 63 |
Quaternion-based Navigation and Control for Small Unmanned Helicopter *
|
Suzuki, Satoshi
|
|
2010
|
43 |
15 |
p. 37-42
6 p.
|
artikel
|
| 64 |
Robust analysis of Demeter benchmark via quadratic separation
|
Peaucelle, Dimitri
|
|
2010
|
43 |
15 |
p. 530-535
6 p.
|
artikel
|
| 65 |
Robust Attitude Control of a Communication Satellite with Large-scale Flexible Antennas *
|
Somov, Ye. I.
|
|
2010
|
43 |
15 |
p. 291-296
6 p.
|
artikel
|
| 66 |
Robust Fault Diagnosis strategies for Spacecraft Application to LISA Pathfinder experiment
|
Falcoz, Alexandre
|
|
2010
|
43 |
15 |
p. 404-409
6 p.
|
artikel
|
| 67 |
Robustness of deadlock avoidance in assembling large-scale structure by multiple robots having trouble and individual differences
|
Otani, Masayuki
|
|
2010
|
43 |
15 |
p. 392-397
6 p.
|
artikel
|
| 68 |
Satellite Design Methodology To Suppress Time-varying Residual Magnet Effects on Attitude For Nano-Satellites
|
Suehiro, Tomoya
|
|
2010
|
43 |
15 |
p. 241-246
6 p.
|
artikel
|
| 69 |
Satellite networks: solutions against emerging space threats
|
Cristini, Frédéric
|
|
2010
|
43 |
15 |
p. 380-385
6 p.
|
artikel
|
| 70 |
Satellite operation improvement through efficient data combination in ground station networks
|
Schmidt, Marco
|
|
2010
|
43 |
15 |
p. 524-530
7 p.
|
artikel
|
| 71 |
Simulation Infrastructure for Autonomous Vision-Based Navigation Technologies
|
Neveu, D.
|
|
2010
|
43 |
15 |
p. 279-286
8 p.
|
artikel
|
| 72 |
Single Modal Vibration Control of Laminated Plates based on the Optimal Placement of a Sensor and an Actuator
|
Kameyama, Masaki
|
|
2010
|
43 |
15 |
p. 235-240
6 p.
|
artikel
|
| 73 |
Singularities of optimal attitude motions
|
Biggs, James D.
|
|
2010
|
43 |
15 |
p. 188-191
4 p.
|
artikel
|
| 74 |
Small Space Debris Sweeper with Probing
|
Ikeuchi, Masayuki
|
|
2010
|
43 |
15 |
p. 184-189
6 p.
|
artikel
|
| 75 |
Smart Algorithms for Astronaut Localization and Navigation on the Surface of Mars Planet Based on Natural constraints
|
Hamza, Benzerrouk
|
|
2010
|
43 |
15 |
p. 511-516
6 p.
|
artikel
|
| 76 |
Smart Control Systems for Next-Generation Autonomous Wing-In-Ground Effect Vehicles
|
Nebylov, Alexander
|
|
2010
|
43 |
15 |
p. 112-117
6 p.
|
artikel
|
| 77 |
Spacecraft Attitude and Body Rate Estimation with Four Star Sensor Heads: Concepts and Ground and On-Orbit Verification Results
|
Miyatake, Katsumasa
|
|
2010
|
43 |
15 |
p. 490-495
6 p.
|
artikel
|
| 78 |
State Estimation and Quick Trajectory Optimization for Air-Launch Rocket
|
Miura, Masashi
|
|
2010
|
43 |
15 |
p. 148-153
6 p.
|
artikel
|
| 79 |
Structured flight control law design using non-smooth optimization
|
Gabarrou, M.
|
|
2010
|
43 |
15 |
p. 536-541
6 p.
|
artikel
|
| 80 |
Table of Contents
|
|
|
2010
|
43 |
15 |
p. i-xii
nvt p.
|
artikel
|
| 81 |
Theory and Software for Simulation of Complex Flexible Aerospace Vehicles and Smart Control
|
Panferov, Alexander I.
|
|
2010
|
43 |
15 |
p. 154-159
6 p.
|
artikel
|
| 82 |
The unified technique for multimode flight control systems designing
|
Borisov, V.G.
|
|
2010
|
43 |
15 |
p. 25-30
6 p.
|
artikel
|
| 83 |
Three-layer Aircraft Control: Path-planning, Guidance, Model Predictive Controller as Autopilot
|
Voelker, A.
|
|
2010
|
43 |
15 |
p. 81-86
6 p.
|
artikel
|
| 84 |
Translational Motion Control for Asymmetric Flexible Satellite and Its Vibration Suppression Effect
|
Nakamura, Tsutomu
|
|
2010
|
43 |
15 |
p. 224-229
6 p.
|
artikel
|
| 85 |
TRON - Hardware-in-the-Loop Test Facility for Lunar Descent and Landing Optical Navigation
|
Krüger, Hans
|
|
2010
|
43 |
15 |
p. 265-270
6 p.
|
artikel
|
| 86 |
Two-dimensional Trajectory Optimization of a Soft Lunar Landing from a Parking Orbit Considering a Landing Site
|
Ahn, Jong-Sun
|
|
2010
|
43 |
15 |
p. 178-183
6 p.
|
artikel
|
| 87 |
UAV Guidance Law for Target Tracking along constrained Bow-Shaped Trajectory based on Lyapunov Vector Field
|
Regina, Niki
|
|
2010
|
43 |
15 |
p. 87-92
6 p.
|
artikel
|
| 88 |
Unscented Batch Sequential Filter and Its Application to Relative Orbit Determination for Formation Flight
|
Tsuda, Yuichi
|
|
2010
|
43 |
15 |
p. 465-471
7 p.
|
artikel
|
| 89 |
Virtual Structure Based Attitude Control of Tether-Controlled Spinning Solar Sail Considering Membrane Vibration
|
Nishida, Junichi
|
|
2010
|
43 |
15 |
p. 356-361
6 p.
|
artikel
|
| 90 |
Vision-based guidance, navigation, and control of Hayabusa spacecraft - Lessons learned from real operation -
|
Hashimoto, Tatsuaki
|
|
2010
|
43 |
15 |
p. 259-264
6 p.
|
artikel
|
| 91 |
Vision Based Navigation for Space Exploration
|
Flandin, G.
|
|
2010
|
43 |
15 |
p. 285-290
6 p.
|
artikel
|
| 92 |
Wind field bounded error identification and robust guidance law design for a small-scaled helicopter
|
Achour, Walid
|
|
2010
|
43 |
15 |
p. 43-48
6 p.
|
artikel
|
| 93 |
Worst-case Analysis of Autonomous Rendezvous Systems
|
Wang, Wenfei
|
|
2010
|
43 |
15 |
p. 321-326
6 p.
|
artikel
|
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