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                             192 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 Accurate Modes Design of the Darwin Precursor Formation Flying Demonstration Mission Charbonnel, Catherine
 2004
 37 6 p. 119-124
6 p.
 artikel
2 A command governor approach to formation flying control problems Bacconi, F.
 2004
 37 6 p. 1085-1090
6 p.
 artikel
3 Active Angular Stabilization of the GAIA Space Telescope Through Laser Interferometry Canuto, Enrico
 2004
 37 6 p. 955-960
6 p.
 artikel
4 Adavance of Chinese Spacecraft Control Technologies Liangdong, Liu
 2004
 37 6 p. 173-178
6 p.
 artikel
5 A Discrete-Time Adaptive Control Scheme Based on Interval Persistency Carrijo, Domingos Sálvio
 2004
 37 6 p. 443-448
6 p.
 artikel
6 Advanced Fuzzy Side Force Control for Missile Against Hypersonic Target Lin, Chun-Liang
 2004
 37 6 p. 641-646
6 p.
 artikel
7 Aeroservoelastic Analysis of Missile Control Surfaces via Robust Control Methods Akmeşe, Alper
 2004
 37 6 p. 719-723
5 p.
 artikel
8 A Formal Approach for Decentralised co-Ordination Among UAVs Using Hybrid Control Jeyaraman, Suresh
 2004
 37 6 p. 1067-1072
6 p.
 artikel
9 Air-Breathing Hypersonic Flight Control 1 Fida, Bariş
 2004
 37 6 p. 559-564
6 p.
 artikel
10 Aircraft Guidance Law Analysis Geri, Walter
 2004
 37 6 p. 499-504
6 p.
 artikel
11 Aircraft-on-Ground Lateral Control for Low Speed Maneuvers Duprez, J.
 2004
 37 6 p. 475-480
6 p.
 artikel
12 A Lyapunov-Typed Nonlinear Attitude Controller for Spacecraft Zhang, J.R.
 2004
 37 6 p. 161-165
5 p.
 artikel
13 A Miniaturised GPS Receiver for Space Applications Ebinuma, Takuji
 2004
 37 6 p. 1103-1106
4 p.
 artikel
14 An Adaptive Tuning Strategy of PID Attitude Control System Abdallah, Yasser M.
 2004
 37 6 p. 1009-1014
6 p.
 artikel
15 An Agent Based Framework for Control of Merging Air-Traffic Heymann, Michael
 2004
 37 6 p. 493-498
6 p.
 artikel
16 An Alternative to Circumvent HJI Computation Difficulty in Nonlinear Robustness Analysis Henni, Assia
 2004
 37 6 p. 707-712
6 p.
 artikel
17 Analytical Method for Computing Controller Gains of a Satellite Launcher Carmona, D.
 2004
 37 6 p. 1019-1023
5 p.
 artikel
18 An Autonomous Celestial Navigation Method for Geosychronous Satellite Xiaolin, Ning
 2004
 37 6 p. 179-183
5 p.
 artikel
19 A New Error Compensation Scheme for INS Vertical Channel Seo, Jaewon
 2004
 37 6 p. 1119-1124
6 p.
 artikel
20 An Improved Recursive Interacting Multi-Model Algorithm Based on Genetic Algorithm Ziliang, Wang
 2004
 37 6 p. 449-454
6 p.
 artikel
21 An Information Fusion Method for Satellite Autonomous Celestial Navigation Jiancheng, Fang
 2004
 37 6 p. 287-291
5 p.
 artikel
22 A Novel Architecture for Magnetic Attitude Control of Gravity Gradient Satellites Astolfi, A.
 2004
 37 6 p. 113-118
6 p.
 artikel
23 An Overview of Compressor Instabilities: Basic Concepts and Control Tavakoli, Saeed
 2004
 37 6 p. 523-528
6 p.
 artikel
24 Application of the Robust Approach to the Problem of Airborne Gravimetry Kulakova, V.I.
 2004
 37 6 p. 907-912
6 p.
 artikel
25 A Proof-of-Concept Approach for Horizontal Take-Off/Landing Rocket Plane Ohkami, Y.
 2004
 37 6 p. 1025-1030
6 p.
 artikel
26 A Rendezvous and Docking Sensor Using a Videometer Strietzel, Roland
 2004
 37 6 p. 753-758
6 p.
 artikel
27 Asynchronous Switching Decentralized Controllers for Spacecraft Formations Smith, Roy S.
 2004
 37 6 p. 1073-1078
6 p.
 artikel
28 A System Identification Approach to Assessing Airline Pilot Skills Chernyshov, Kirill
 2004
 37 6 p. 535-540
6 p.
 artikel
29 Author Index 2004
 37 6 p. 1147-1149
3 p.
 artikel
30 Automatically Controlled Ekranoplanes: Experience and Problems Vasilevsky, Igor
 2004
 37 6 p. 505-510
6 p.
 artikel
31 Automatic Real-Time Star Detection Technique Romashina, L.V.
 2004
 37 6 p. 815-819
5 p.
 artikel
32 Autonomous Navigation Concepts for Interplanetary Missions Polle, B.
 2004
 37 6 p. 203-208
6 p.
 artikel
33 Autonomous Orbit Control Strategy for Accurate Large Delta-V Manoeuvres in Planck Spinning S/C Zorita, Demetrio
 2004
 37 6 p. 315-320
6 p.
 artikel
34 Autonomous Parafoil Control Experiment as “Comeback Competition” for Effective First Step Training Towards Satellite Development Nakasuka, Shinichi
 2004
 37 6 p. 919-924
6 p.
 artikel
35 Autonomous Robot Navigation Using Traversability Indices Seraji, Homayoun
 2004
 37 6 p. 339-344
6 p.
 artikel
36 Autopilot Design for Agile Missile Using Time-Varying Control Technique Lee, Ho Chul
 2004
 37 6 p. 665-670
6 p.
 artikel
37 Avionic of Fifth-Generation for Seekers of Smart Weapon Antsev, G.V.
 2004
 37 6 p. 647-651
5 p.
 artikel
38 AWIATOR's Study of a Wing Load Control: Design and Flight-Test Results Jeanneau, Matthieu
 2004
 37 6 p. 469-474
6 p.
 artikel
39 3-Axes Attitude Estimation Experiments Using CCD Earth Sensor Sekignchi, Takeshi
 2004
 37 6 p. 741-746
6 p.
 artikel
40 Capabilities of Multiagent-Based Cargo Layout System for H-II Transfer Vehicle Takadama, Keiki
 2004
 37 6 p. 251-256
6 p.
 artikel
41 Cognitive Tools for Humanoid Robots in Space Sofge, Donald
 2004
 37 6 p. 351-356
6 p.
 artikel
42 Commercial Use of GNSS Signals in GEO Mittnacht, M.
 2004
 37 6 p. 1097-1102
6 p.
 artikel
43 Comparison of H-inf and Coefficient Diagram Method in Aerospace Manabe, Shunji
 2004
 37 6 p. 387-392
6 p.
 artikel
44 Computer Aided Modelling and Analytical Synthesis of Control Algorithms for a Spacecraft with Discretely Changing Structure Zemlyakov, S.D.
 2004
 37 6 p. 411-416
6 p.
 artikel
45 Condition Monitoring of Gas Turbine Engine Transmission Rutkovsky, V.Yu.
 2004
 37 6 p. 1037-1042
6 p.
 artikel
46 Control and Navigation Aspects of the New ESA Earth Observation Missions Silvestrin, Pierluigi
 2004
 37 6 p. 13-24
12 p.
 artikel
47 Control Aspects of Aerospace Plane Docking and Undocking with Moving Ekranoplane Nebylov, A.V.
 2004
 37 6 p. 997-1002
6 p.
 artikel
48 Control Design for F-16 Longitudinal Motion Abdullah, Ali A.
 2004
 37 6 p. 529-534
6 p.
 artikel
49 Controller Design in Presence of Non-Smooth Nonlinearity: A Flight Control Example Yurkevich, Valery D.
 2004
 37 6 p. 487-492
6 p.
 artikel
50 Control of the Times of Engine Shutdown by the Launch Safety Criterion Ivanov, V.P.
 2004
 37 6 p. 275-279
5 p.
 artikel
51 Control System of the Microsatellite “Micron” Konyukbov, S.N.
 2004
 37 6 p. 65-70
6 p.
 artikel
52 Corrections of a Vestibular Function Under Extreme Conditions of the Aerospace Flight Alexandrov, V.
 2004
 37 6 p. 269-274
6 p.
 artikel
53 Correlated Fault Modelling for Diagnostics and Monitoring of GTE Control Systems Pashkevich, A.
 2004
 37 6 p. 1031-1036
6 p.
 artikel
54 Current Status of Japanese Aerospace Programs - Focusing on the High Speed Flight Demonstration Miyazawa, Yoshikazu
 2004
 37 6 p. 25-36
12 p.
 artikel
55 3-D Biased PNG for Evasive Maneuver of Anti-Ship Missiles Against CIWS Kim, Yoon-Hwan
 2004
 37 6 p. 659-664
6 p.
 artikel
56 Decentralized Iterative Learning Control Schemes for Large Scale Systems Including Delayed State Perturbations in the Interconnections Wu, Hansheng
 2004
 37 6 p. 381-386
6 p.
 artikel
57 DEIS UAV: GNC Design and Avionics Implementation Issues Crisci, M.
 2004
 37 6 p. 747-752
6 p.
 artikel
58 Design and Analysis of Helicopter Fault-Tolerant Flight Control System Al-Malki, M.F.
 2004
 37 6 p. 885-890
6 p.
 artikel
59 Development and Evaluation of Fault-Tolerant Flight Control for RLV by Mutual Compensation with Available Aerosurfaces Shimura, Koji
 2004
 37 6 p. 849-854
6 p.
 artikel
60 Development of a Condition Monitoring Module for Aircraft Engines and it's Experimental Investigation Arkov, V.
 2004
 37 6 p. 1061-1066
6 p.
 artikel
61 Development of Attitude Control System of Micro LabSat Yoshihara, Keisuke
 2004
 37 6 p. 131-136
6 p.
 artikel
62 Development of Navigation Algorithm Architecture for Automatic Landing Based on Landmarks Image Processing Hyun, Young Mok
 2004
 37 6 p. 257-262
6 p.
 artikel
63 Differential Geometric Guidance Based on the Involute of the Target's Trajectory: 3-D Aspects Ariff, Omar
 2004
 37 6 p. 605-610
6 p.
 artikel
64 3D Nonlinear H2/H∞ Adaptive Guidance Law for Homing Missiles Chen, Hsin-Yuan
 2004
 37 6 p. 583-586
4 p.
 artikel
65 Dynamical Analysis for Task Configuration of Redundant Flexible Space Manipulator on Space Platform Komats, Tadashi
 2004
 37 6 p. 363-368
6 p.
 artikel
66 Dynamic Models of Comprehensive Scheduling for Ground-Based Facilities Communication with Navigation Spacecrafts Sokolov, B.V.
 2004
 37 6 p. 263-268
6 p.
 artikel
67 Dynamics of Coupled Flap-Lag Motion by the Helicopter Rotor Blades Mikhailov, S.A.
 2004
 37 6 p. 565-570
6 p.
 artikel
68 Electric Propulsions as Actuators of the Spacecraft Flight Control Systems Antropov, N.N.
 2004
 37 6 p. 229-234
6 p.
 artikel
69 End-to-End Modeling for Drag-Free Missions with Application to LISA Pathfinder Brandt, Nico
 2004
 37 6 p. 241-246
6 p.
 artikel
70 Energy Speed-Gradient Control of Satellite Oscillations Fradkov, Alexander
 2004
 37 6 p. 417-422
6 p.
 artikel
71 ENVISAT Payload Operations Planning - The End-To-End View And Experience Diekmann, Frank J.
 2004
 37 6 p. 305-310
6 p.
 artikel
72 Experimental Demonstration of Coordinated Control for Multi-Vehicle Teams King, Ellis
 2004
 37 6 p. 345-350
6 p.
 artikel
73 Experimental Evaluation of the Micro-Tech.-Sensor for Attitude and Orbit Determination Kuehl, Christopher
 2004
 37 6 p. 771-776
6 p.
 artikel
74 Explicit Guidance for an Oblate Gravitational Field Shahzad, Amir
 2004
 37 6 p. 461-467
7 p.
 artikel
75 Extended Parity Space Approach Considering Two-Faults Kim, Kwang Hoon
 2004
 37 6 p. 879-884
6 p.
 artikel
76 Extensive Comparison Between Quantitative Pursuit Evasion Game Guidance Law and PNS Le Ménec, Stéphane
 2004
 37 6 p. 611-615
5 p.
 artikel
77 Fault Detection and Diagnosis of a Linear Hydraulic Servo Axis Muenchhof, Marco
 2004
 37 6 p. 861-866
6 p.
 artikel
78 FDI Algorithms for GPS Signals: A Different Perspective of a Known Problem Castaldi, P.
 2004
 37 6 p. 1107-1112
6 p.
 artikel
79 FDI for Inertial Sensor using Single Antenna GPS Receiver Kim, Young Jin
 2004
 37 6 p. 867-871
5 p.
 artikel
80 Feedback Controller Design for the Basic Science Mode of the LISA Pathfinder Mission Gathl, Peter
 2004
 37 6 p. 839-844
6 p.
 artikel
81 Feedback Control of MEMS Gyroscope to Achieve the Tactical-Grade Specifications Park, Yonghwa
 2004
 37 6 p. 671-676
6 p.
 artikel
82 Filtering, Prediction and Smoothing with Point-Mass Approach Královec, Jakub
 2004
 37 6 p. 375-380
6 p.
 artikel
83 Flexible Launch Vehicle Attitude Control Design Using Coevolutionary Algorithm Lee, Hyunjae
 2004
 37 6 p. 979-984
6 p.
 artikel
84 Flight Data Analysis of ADEOS-II GPS Receivers Ito, Toshio
 2004
 37 6 p. 1113-1118
6 p.
 artikel
85 Flight Evaluation of GPS Aided Inertial-Navigation Avionics with GBAS and SBAS Augmentation Harigae, Masatoshi
 2004
 37 6 p. 1137-1142
6 p.
 artikel
86 Formation of Special Balance Mode for a Return Space Vehicle in Dynamics of Atmospheric Descent Afanasyev, V.A.
 2004
 37 6 p. 311-314
4 p.
 artikel
87 Gas-Turbine Engine Control System of the Unmanned Airplane Kulik, A.S.
 2004
 37 6 p. 1049-1053
5 p.
 artikel
88 GLONASS/GPS Monitoring Equipment Bogdanov, P.P.
 2004
 37 6 p. 1143-1146
4 p.
 artikel
89 Graph Models of Orbital Assembly and Dynamics of a Large Space Structure Rutkovsky, V.Yu.
 2004
 37 6 p. 77-82
6 p.
 artikel
90 High-Precision Attitude Control of Remote Sensing Satellite Lebedev, D.V.
 2004
 37 6 p. 735-740
6 p.
 artikel
91 High-Precision Navigation and Guidance Systems of Aerial Vehicles is the Use of Computer Vision Technologies Fedosov, E.
 2004
 37 6 p. 587-592
6 p.
 artikel
92 Hybrid Model for Receding Horizon Guidance of Agile Autonomous Rotorcraft Schouwenaars, Tom
 2004
 37 6 p. 481-486
6 p.
 artikel
93 Influence of Time Delay on Engagement Process Under Proportional Navigation Law Alexandrov, V.V.
 2004
 37 6 p. 433-436
4 p.
 artikel
94 Integrated Guidance and Control of Missiles with θ-D Method Xin, Ming
 2004
 37 6 p. 629-634
6 p.
 artikel
95 Integrated Modular Spacecraft Avionics. Architecture and SpaceWire-Based Implementation Sbeynin, Yuriy
 2004
 37 6 p. 799-804
6 p.
 artikel
96 Integrated Power and Attitude Control Using VSCMGs for Agile Small Agile Satellite Liang, Tang
 2004
 37 6 p. 167-172
6 p.
 artikel
97 Integrated Sensor/Actuator FDI Based on RKF Insensitive to Sensor Failures Hajiyev, Chingiz
 2004
 37 6 p. 765-770
6 p.
 artikel
98 Invariant and Periodic Filters for Helicopter Vibration Attenuation Lovera, M.
 2004
 37 6 p. 517-522
6 p.
 artikel
99 Investigation of Genetic Algorithms On-Line Application for Aero Engine Modelling and Condition Monitoring Breikin, T.V.
 2004
 37 6 p. 1043-1047
5 p.
 artikel
100 Kansas Universities' Technology Evaluation Satellite Program Sorensen, Trevor C.
 2004
 37 6 p. 937-941
5 p.
 artikel
101 LAAS Ground Facility and Navigation Virtual Laboratory Integration Aspects: A Mixed Real/Simulated Environment to Test DGNSS Avionics Crisci, M.
 2004
 37 6 p. 1131-1136
6 p.
 artikel
102 Launcher Attitude Control: Some Answers to the Robustness Issue Imbert, Nicole
 2004
 37 6 p. 961-966
6 p.
 artikel
103 Lessons Learned from the Object-Oriented Design of the BIRD Attitude Control System Software Maibaum, Olaf
 2004
 37 6 p. 155-160
6 p.
 artikel
104 Linearization and Identification of Aircraft Turbofan Engine Models Henrion, Didier
 2004
 37 6 p. 1055-1060
6 p.
 artikel
105 Load Relief Control of H-IIA Launch Vehicle Suzuki, Hideto
 2004
 37 6 p. 985-990
6 p.
 artikel
106 Logic and Numerical Methods of Spacecraft Attitude Control and Reconfiguration Vassilyev, S.N.
 2004
 37 6 p. 399-404
6 p.
 artikel
107 Longitudinal Anisotropy-Based Flight Control in a Wind Shear Kurdyukov, A.P.
 2004
 37 6 p. 423-426
4 p.
 artikel
108 Mathematical Models and Software for Flexible Vehicle Simulation Brodsky, Sergey
 2004
 37 6 p. 973-978
6 p.
 artikel
109 McflightmTM-Systems-on-Chip for Aerospace Applications Solokhina, Tatiana
 2004
 37 6 p. 827-832
6 p.
 artikel
110 Measuring Microaccelerations Aboard Spacecrafts Mumin, O.L.
 2004
 37 6 p. 845-848
4 p.
 artikel
111 Mechanics and Motion Control of a Space Vehicle in the Project of Relict Substance Delivery on Earth (the Project "Phobos_Grunt") Akim, E.L.
 2004
 37 6 p. 209-214
6 p.
 artikel
112 Method of Conflict-Optimum Guidance of the Wing of Two Aircrafts on the Basis of the Stable-Effective Compromise Voronov, E.M.
 2004
 37 6 p. 925-930
6 p.
 artikel
113 Micro-Gravity Isolation using Only Electo-Magnetic Actuators Alminde, Lars
 2004
 37 6 p. 913-918
6 p.
 artikel
114 Micro Sun Sensor for Spacecraft Attitude Control Mobasser, Sohrab
 2004
 37 6 p. 833-838
6 p.
 artikel
115 Microvibration Management and Pointing Stability Analysis of SELENE Satellite Kamiya, Tosbio
 2004
 37 6 p. 143-148
6 p.
 artikel
116 Model-Based Fault Detection and Diagnosis - Status and Applications Isermann, Rolf
 2004
 37 6 p. 49-60
12 p.
 artikel
117 Modelling and Simulation of Flexibility Induced Disturbances for a Flying Rocket Anwar Mughal, M.
 2004
 37 6 p. 1015-1018
4 p.
 artikel
118 Modelling Real-Time Behaviour of Soft Computations within Integrated Avionics Systems McElhone, Charlie
 2004
 37 6 p. 787-792
6 p.
 artikel
119 Multi-Objective Frequency Loop-Shaping of a Lateral Missile Autopilot Sreenuch, T.
 2004
 37 6 p. 577-582
6 p.
 artikel
120 National Achievements in Control Theory (The Aerospace Perspective) Krotov, V.F.
 2004
 37 6 p. 37-48
12 p.
 artikel
121 New Direction on Robotic Hands Design for Space Applications Biagiotti, L.
 2004
 37 6 p. 327-332
6 p.
 artikel
122 Nonlinear Dynamics of a Gyroplane Rotor * Somov, Yevgeny I.
 2004
 37 6 p. 553-558
6 p.
 artikel
123 Nonlinear Dynamics of a Spacecraft Respinup by a Weak Internal Control Somov, Ye.I.
 2004
 37 6 p. 95-100
6 p.
 artikel
124 Nonlinear Filtering, Interpolation and Extrapolation in Stochastic Systems Under Continuous and Discrete Observations with Memory Dyomin, N.S.
 2004
 37 6 p. 809-814
6 p.
 artikel
125 Nutation Stability Study of Flywheel Rotor Supported by AMB Shucheng, Dong
 2004
 37 6 p. 805-808
4 p.
 artikel
126 Observability Analysis of a Geostationary Satellite Autonomous Navigation System Jianxin, Guo
 2004
 37 6 p. 281-285
5 p.
 artikel
127 Onboard Control Complex for Vehicles Implementation Concept by ISS Example Chertok, B.
 2004
 37 6 p. 107-111
5 p.
 artikel
128 On-Line Evolutionary Algorithm Guidance for Multiple Missiles Against Multiple Targets Hughes, Evan J.
 2004
 37 6 p. 1091-1096
6 p.
 artikel
129 On-Orbit Experiment of Motion Estimation and Tracking of Tumbling Object in Space Nakasuka, Shinichi
 2004
 37 6 p. 223-228
6 p.
 artikel
130 On-Orbit Operation and Performance of Micro LabSat Attitude Control Subsystem Yamamoto, Toru
 2004
 37 6 p. 89-94
6 p.
 artikel
131 On the Optimal Estimator of Randomly Maneuvering Targets for Terminal Guidance Shinar, Josef
 2004
 37 6 p. 571-576
6 p.
 artikel
132 On the Precision Attitude Control Problems Branets, V.
 2004
 37 6 p. 61-64
4 p.
 artikel
133 On the Refinement of Discretization for Optimal Control Problems Laurent-Varin, Julien
 2004
 37 6 p. 405-410
6 p.
 artikel
134 Optimal Guidance Law for Impact Angle Control Song, Chanho
 2004
 37 6 p. 653-658
6 p.
 artikel
135 Orbit Acquisition of the Disaster Monitoring Constellation – Preliminary Results Imre, Egemen
 2004
 37 6 p. 215-221
7 p.
 artikel
136 Orbit Dynamics and Kinematics with Full Quaternions Andreis, Davide
 2004
 37 6 p. 185-190
6 p.
 artikel
137 Organization of an Intellectual Technological Searching Cycle to Support Making Decisions During a Space Vehicles (SV) Remote Control Lev, Bocharov
 2004
 37 6 p. 247-249
3 p.
 artikel
138 Overview of Recent Control Technology for Japanese Scientific Space Missions Ninomiya, Keiken
 2004
 37 6 p. 191-196
6 p.
 artikel
139 Overview of the Attitude and Orbit Control Systems (AOCS) Developed for NASDA/JAXA Engineering Test and Applications Satellites Ohkami, Yoshiaki
 2004
 37 6 p. 197-202
6 p.
 artikel
140 Position Control Design and Validation Applied to ATV During Docking to ISS Bourdon, Jérôme
 2004
 37 6 p. 83-88
6 p.
 artikel
141 Preface Nebylov, Alexander
 2004
 37 6 p. iv-
1 p.
 artikel
142 Preliminary Tests of GPS/HAPS Positioning System Using a Pseudolite on Helicopter Tsujii, T.
 2004
 37 6 p. 1125-1130
6 p.
 artikel
143 Problem of Optimal Control of the Local System of Aircrafts (LSA) Resources on the Basis of the Game Forecast Voronov, E.M.
 2004
 37 6 p. 541-545
5 p.
 artikel
144 QFT/H∞ Control of a Small Solar Thermal Transfer Vehicle (SOTV) with Inflatable Appendages Drail, Rémi
 2004
 37 6 p. 677-682
6 p.
 artikel
145 Quantitative Feedback Theory Applied to Orbital Rendezvous Ganet-schoeller, Martine
 2004
 37 6 p. 321-326
6 p.
 artikel
146 Regulated Air Traffic Flow Simulation Tool Degtyaryev, O.V.
 2004
 37 6 p. 547-552
6 p.
 artikel
147 Residual Generator Computation for Fault Detection of a General Aviation Aircraft Bonfè, M.
 2004
 37 6 p. 873-878
6 p.
 artikel
148 Robot/Balloon Facility for Autonomous Robotic Grasping of Objects in Space Sharf, Inna
 2004
 37 6 p. 369-374
6 p.
 artikel
149 η-Robust Algorithms of Flight Control on Variable Asymmetrical Limitations Pilishkin, V.N.
 2004
 37 6 p. 427-432
6 p.
 artikel
150 Robust Computer Image Analysis for Flight Vehicles Navigation and Guidance Zheltov, Sergey Yu.
 2004
 37 6 p. 725-728
4 p.
 artikel
151 Robust Control of a Space Launcher by Introducing LQG/LTR Ideas in the NCF Robust Stabilisation Problem Abbas-Turki, Mohamed
 2004
 37 6 p. 1003-1008
6 p.
 artikel
152 Robust Digital Control of Drag-Free Satellites Canuto, Enrico
 2004
 37 6 p. 683-688
6 p.
 artikel
153 Robust GPS C/A Code Tracking Based on H∞ Control Jee, Gyu-In
 2004
 37 6 p. 729-734
6 p.
 artikel
154 Robust Impulse-to-Peak Synthesis: Application to the Control of an Aerospace Launcher Arzelier, D.
 2004
 37 6 p. 967-972
6 p.
 artikel
155 Robustness Analysis of a Nonlinear Missile Autopilot via Integral Quadratic Constraints Adounkpé, Ifédé-Joël
 2004
 37 6 p. 713-718
6 p.
 artikel
156 Robust Nonlinear Control of a Spacecraft during Landing Maneuvers on a Planet Henni, Assia
 2004
 37 6 p. 689-694
6 p.
 artikel
157 ROKVISS - Space Robotics Dynamics and Control Performance Experiments at the ISS Schäfer, Bernd
 2004
 37 6 p. 333-338
6 p.
 artikel
158 Russian Multifunctional Education-Research Students' Satellite "Mozhaetz" on the Orbit Fateev, V.
 2004
 37 6 p. 897-900
4 p.
 artikel
159 Russian Space Programs: Achievements and Prospects of Automatic Control Applications Legostaev, Victor P.
 2004
 37 6 p. 1-12
12 p.
 artikel
160 Sample Size Adaptation for Particle Filters Straka, Ondřej
 2004
 37 6 p. 437-442
6 p.
 artikel
161 Semi-Active Vibration Isolation System for Launch Vehicles Iwamoto, Kousuke
 2004
 37 6 p. 991-996
6 p.
 artikel
162 Sensor Fault Diagnosis of Singularly Perturbed Systems Applied to F-8 Flight Dynamic Tellili, Adel
 2004
 37 6 p. 855-860
6 p.
 artikel
163 Shunting Method for Control of Homing Missiles with Uncertain Parameters Fradkov, Alexander
 2004
 37 6 p. 593-598
6 p.
 artikel
164 Single-Pulse Correction of the Re-Entry Point of a Payload Module Andrievsky, Boris
 2004
 37 6 p. 235-239
5 p.
 artikel
165 Some Problems of Design of Computer-Based Training Systems for Civil Aviation Pilots, Methods of their Solving Popov, O.
 2004
 37 6 p. 511-515
5 p.
 artikel
166 Spacecraft Disposal on a Graveyard Orbit: The In-Flight AOCS Performance for Eurostar 2000 and SPOT 1 during End-of-Life Operations Mignon, D.
 2004
 37 6 p. 125-130
6 p.
 artikel
167 SpaceWire Satellite Onboard Data-Handling Networks Parkes, Steve
 2004
 37 6 p. 759-764
6 p.
 artikel
168 Stationkeeping and Slewing Control of a Multi-Tethered Aerostat Gilardi, Gabriele
 2004
 37 6 p. 777-782
6 p.
 artikel
169 Steering the Control Moment Gyroscope Clusters Onboard High-Agile Spacecraft * Somov, Ye.I.
 2004
 37 6 p. 137-142
6 p.
 artikel
170 Synergy in Power and Momentum Management for Spacecraft Using Double Gimbaled Solar Arrays auf der Heide, K.
 2004
 37 6 p. 293-298
6 p.
 artikel
171 Synthesis of Optimal and Suboptimal Adaptive Control Systems Under Bounded Disturbances Kuntsevich, Vsevolod M.
 2004
 37 6 p. 393-398
6 p.
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172 Systematic Approach to Achieve Fine Pointing Requirement of SOLAR-B Yoshida, Norimasa
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173 System Design and Attitude Control Analyses for the Pico-Satellite UWE-1 Fullmer, Rees
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174 Target Arrival Coordination in Boid Based Formation Flight Park, Chang-Su
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175 Terminal Missile Guidance Using a Semi-Markov Target Model Dionne, Dany
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176 The AAU-Cubesat Student Satellite Project: Architectural Overview and Lessons Learned Alminde, Lars
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177 The Autonomous Constellation Formation-Keeping Control Exploiting Orbital Maneuver Efficiency Honghua, Zhang
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178 The Conception of Electric Propulsion Systems Vector Control Galka, Victor
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179 The Data Flow and Distributed Calculations Intelligence Information Technology for Decision Support Embeded System in Real Time Okhtilev, Michael Yu.
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180 The Generalized (μ,MU)-Iteration Illustrated by Flexible Aircraft Robust Control Kron, Aymeric
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181 The Multiple Hypothesis Extension of the Information Set-Based Tracking Algorithm for Multi-Target Environment Emeliyanov, Dmitry D.
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182 The Problems of Characteristic Stabilization for Micromechanical Gyroscopes Severov, L.A.
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183 The Spatial Reconstruction of Earth Surface by Stereoimages Ryabokon, Dmitry
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184 The μ-Synthesis Applied to a Launcher Control Morita, Y.
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185 Three DOF Optimal Thrusters Selection and Modulation for Space Vehicles Silva, N.
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186 Tokyo Tech 1kg Pico-Satellite CUTE-I-Development, Launch & Operations Omagari, Kuniyuki
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187 Trajectory Control of Autonomous Vehicles in Viscous Media 1 Miroshnik, Iliya V.
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188 Unified Approach for Open-Loop Optimal Control with Applications to Aerospace Systems Imura, Yoshiko
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189 University of Tokyo's Student Nano-Satellite Project CubeSat-XI and Its On-Orbit Experiment Results Funase, R.
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190 Variable Speed Missile Guidance Law Against a Maneuvering Target Dohi, Naoto
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191 Visual Feedback Attitude Control Experiment of a Bias Momentum Micro Satellite Terui, Fuyuto
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192 Zero Miss Interception Guidance: Cheap Control Approach Turetsky, Vladimir
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                             192 gevonden resultaten
 
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