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                             91 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 Algorithm of Federated Filter With Different Local and Master Filter States Qiu, Hong Zhuan
 2001
 34 15 p. 253-258
6 p.
 artikel
2 An Application of the µ-Synthesis to Launcher Attitude Control Design Morita, Yasuhiro
 2001
 34 15 p. 123-128
6 p.
 artikel
3 An Improved LWR Method For On-Line Aircraft Parameter Identification Campa, Giampiero
 2001
 34 15 p. 99-104
6 p.
 artikel
4 Application of Coefficient Diagram Method to Dual-Control-Surface Missile Manabe, Shunji
 2001
 34 15 p. 499-504
6 p.
 artikel
5 Arbitrary Fuel-Optimal Attitude Maneuvering of Non-Symmetric Space Vehicle in a Connected Frame Ioslovich, Ilya
 2001
 34 15 p. 32-36
5 p.
 artikel
6 A Robust Multi-Objective Synthesis Applied to Launcher Attitude Control Voinot, Olivier
 2001
 34 15 p. 203-208
6 p.
 artikel
7 Attitude Determination With GPS Based on Predictive Filter Yang, Jing
 2001
 34 15 p. 247-252
6 p.
 artikel
8 A Two Input Tracking Autopilot During Target Acquisition Asthana, Chandra B.
 2001
 34 15 p. 155-160
6 p.
 artikel
9 A Two-Level Optimal Estimator for Attitude Determination Using GPS Measurements Li, Yong
 2001
 34 15 p. 235-240
6 p.
 artikel
10 Autonomous Predicted Control of Spacecraft with Changing Configuration Zemlyakov, S.D.
 2001
 34 15 p. 91-96
6 p.
 artikel
11 A Virtual Laboratory for Space Systems Engineering Experiments Schilling, K.
 2001
 34 15 p. 326-331
6 p.
 artikel
12 A Virtual Laboratory on Satellite-Based Navigation Crisci, M.
 2001
 34 15 p. 283-288
6 p.
 artikel
13 Calibration of Time Synchronization Error in GPS/SDINS Hybrid Navigation Lee, Hyung Keun
 2001
 34 15 p. 223-228
6 p.
 artikel
14 Cassa-Concept of Active System Safety for Aviation Schagaev, Igor
 2001
 34 15 p. 320-325
6 p.
 artikel
15 Complexity Mitigation By Active Control Applied to Linear Dynamic Systems Bukley, Angelia P.
 2001
 34 15 p. 161-166
6 p.
 artikel
16 Control of Input Redundant Affine Systems: Application to Runway Axis Tracking at Landing Villaumé, F.
 2001
 34 15 p. 338-343
6 p.
 artikel
17 Control System Investigation by Means of Dynamically Similar Models Sadovnychiy, S.
 2001
 34 15 p. 67-72
6 p.
 artikel
18 Design and Flight Test of a Robust Autopilot for the IRIS-T Air-To-Air Missile Buschek, Harald
 2001
 34 15 p. 449-454
6 p.
 artikel
19 Design Of Parameteric Adaptive Controller For Mimo Differential Algebraic Systems 1 Wang, Jie
 2001
 34 15 p. 209-214
6 p.
 artikel
20 Design of Self-Organizing Fuzzy Logic Guidance Law Lin, Chih-Min
 2001
 34 15 p. 396-403
8 p.
 artikel
21 Dynamic Compensation for a Rotational Motion Simulator Funada, A.S.
 2001
 34 15 p. 507-511
5 p.
 artikel
22 Dynamics and Control of Tethered Satellite System 1 Yu, Shaohua
 2001
 34 15 p. 141-146
6 p.
 artikel
23 Dynamics of the Maneuvering Vehicle Ikar Control System by the Orbital Placement of Globalstar satellites ⋆ Somov, Ye.I.
 2001
 34 15 p. 372-377
6 p.
 artikel
24 Evaluation of Timing and Fault Handling Qualities of Distributed Flight Control System Ahlström, Kristina
 2001
 34 15 p. 308-313
6 p.
 artikel
25 Exclusive and Non-Exclusive Multi-Model Tracking Filters For Air Traffic Control Kowalczuk, Zdzisław
 2001
 34 15 p. 135-140
6 p.
 artikel
26 Fine Gyroless Attitude Control: The Sax Experience Martella, P.
 2001
 34 15 p. 37-46
10 p.
 artikel
27 Flight Control Design For A STT Missile: A Fuzzy LPV Approach Blumel, Anna V.
 2001
 34 15 p. 455-460
6 p.
 artikel
28 Flight Data Analysis and Calibration of Optical Sensors for Geostationary Missions * Juckenhoefel, O.
 2001
 34 15 p. 19-
1 p.
 artikel
29 Fodias Project: An Overview and the Development Status (*) Benatti, M.
 2001
 34 15 p. 282-
1 p.
 artikel
30 Future Technology for Flight Control Systems Torin, Jan
 2001
 34 15 p. 332-337
6 p.
 artikel
31 Fuzzy Adaptive Kalman Filtering for INS/GPS Data Fusion and Accurate Positioning Sasiadek, J.Z.
 2001
 34 15 p. 410-415
6 p.
 artikel
32 Gain Scheduling for an Aerospace Launcher With Bending Modes Clement, Benoît
 2001
 34 15 p. 475-480
6 p.
 artikel
33 Generalized Derivation of The EKF Based Inertial Navigation Error Dynamics Eck, Christoph
 2001
 34 15 p. 259-264
6 p.
 artikel
34 H-IIA Rocket Range Safety - GPS Application Miyano, Tomoyuki
 2001
 34 15 p. 229-234
6 p.
 artikel
35 Improved Filter Type Integrity Monitoring In Satellite Navigation Yang, Wen-Chieh
 2001
 34 15 p. 217-222
6 p.
 artikel
36 Increase of Positioning Robustness By Integration of CDMA and GPS Kim, Wuk
 2001
 34 15 p. 270-275
6 p.
 artikel
37 INS/GPS Integration Using Parallel Kalman Filtering Hajiyev, Chingiz
 2001
 34 15 p. 512-517
6 p.
 artikel
38 Integrating Satellite and Inertial Navigation-Conventional and New Fusion Approaches Wagner, Joerg F.
 2001
 34 15 p. 241-246
6 p.
 artikel
39 Internal-Model-Based Control of Nonlinear Systems Isidori, Alberto
 2001
 34 15 p. 3-
1 p.
 artikel
40 Large Space Structures: Modelling and Control Anshakov, Gennady
 2001
 34 15 p. 303-307
5 p.
 artikel
41 List of Authors 2001
 34 15 p. 549-551
3 p.
 artikel
42 Longitudinal Flight Control System Design for Propulsion Controlled Aircraft Ochi, Yoshimasa
 2001
 34 15 p. 314-319
6 p.
 artikel
43 LPV Model Identification For The Stall And Surge Control of a Jet Engine Bamieh, B.
 2001
 34 15 p. 105-110
6 p.
 artikel
44 LQG Vibration Control for Plate Structures Using Piezoceramic Transducers Iorga, L.
 2001
 34 15 p. 518-524
7 p.
 artikel
45 Magnetometer Use in Momentum Bias Systems Fichter, Walter
 2001
 34 15 p. 20-25
6 p.
 artikel
46 Methods and Software for Research and Design of Spacecraft Robust Fault Tolerant Control Systems * Somov, Ye.I.
 2001
 34 15 p. 5-16
12 p.
 artikel
47 Minimizing Radar Exposure in Air Vehicles Path Planning * Pachter, Meir
 2001
 34 15 p. 526-530
5 p.
 artikel
48 Missile Guidance Laws Based on Pursuit-Evasion Game Formulations Shinar, Josef
 2001
 34 15 p. 437-442
6 p.
 artikel
49 Modelling, Control and Simulation OD a Light Twin-Engine Aircraft * Mazzoni, S.
 2001
 34 15 p. 525-
1 p.
 artikel
50 Modern Missile Flight Control Design: An Overview Tsourdos, Antonios
 2001
 34 15 p. 425-430
6 p.
 artikel
51 Modern Missile Guidance Design: An Overview White, Brian A.
 2001
 34 15 p. 431-436
6 p.
 artikel
52 Navigation Sensors Architecture for the Automated Transfer Vehicle Dussy, Stéphane
 2001
 34 15 p. 365-371
7 p.
 artikel
53 Neural Aircraft Autopilot Gain Adjuster Raimbault, Nathalie
 2001
 34 15 p. 404-409
6 p.
 artikel
54 Neural Network-Based Virtual Sensors In Flight Control Systems Tranchero, Bruno
 2001
 34 15 p. 416-421
6 p.
 artikel
55 Nonlinear Disturbance Observer Based Dynamic Inversion Control of Missiles Chen, Wen-Hua
 2001
 34 15 p. 463-468
6 p.
 artikel
56 Nonlinear Dynamics of Gyromoment Attitude Control and Precise Antenna Pointing by the Sesat Spacecraft * Titov, G.P.
 2001
 34 15 p. 73-78
6 p.
 artikel
57 Nonlinear Six-Degree-of-Freedom Control for Flexible Spacecraft Yamashita, Toshiaki
 2001
 34 15 p. 344-349
6 p.
 artikel
58 One Step Parameter Identification Using Moving Horizon States Estimation Method Legowo, Ari
 2001
 34 15 p. 265-269
5 p.
 artikel
59 Optical Correlator for Image Motion Compensation in the Focal Plane of a Satellite Camera Janschek, K.
 2001
 34 15 p. 378-382
5 p.
 artikel
60 Output Integral Sliding Mode Controllers for Acceleration of a Missile System With Parameter Perturbations Jafarov, Elbrous M.
 2001
 34 15 p. 487-492
6 p.
 artikel
61 Parity Vector Compensation for Fault Diagnosis of Inertial Sensor Unit Ling Wei, Chun
 2001
 34 15 p. 350-355
6 p.
 artikel
62 Passivity Based Nonlinear Attitude Control of the Rømer Satellite Quottrup, Michael Melholt
 2001
 34 15 p. 85-90
6 p.
 artikel
63 PD-Eigenstructure Assignment For Linear Time-Varying Systems and its Application to Missile Flight control Choi, Jae Weon
 2001
 34 15 p. 469-474
6 p.
 artikel
64 Precision Gyro-Stabilized Platform On The Base Of Gas-Static Supported Gyros Alexandrov, Y.S.
 2001
 34 15 p. 47-52
6 p.
 artikel
65 QFT Based Robust Controller Design for Launch Vehicle Autopilot Lalithambika, V.R.
 2001
 34 15 p. 531-535
5 p.
 artikel
66 Quadratic Stabilization With Partial Eigenstructure Assignment: Application To Flight Control Design Satoh, Atsushi
 2001
 34 15 p. 179-184
6 p.
 artikel
67 Rate-Profiler Based Minimum-Time Control for Spacecraft Attitude Manoeuver Saitoh, Tetsu
 2001
 34 15 p. 53-60
8 p.
 artikel
68 Regulation of Rigid Spacecraft Angular Momentum Using Port Controlled Hamiltonian Structure Siguerdidjane, Houria
 2001
 34 15 p. 147-152
6 p.
 artikel
69 Robust Avionics Dead Reckoning Filtering Scheme Via LMI Castaldi, Paolo
 2001
 34 15 p. 276-281
6 p.
 artikel
70 Robust Control Law Design for a Small Commercial Aircraft Amato, F.
 2001
 34 15 p. 297-302
6 p.
 artikel
71 Robust Control of the Missile Attitude Based on Quaternion Feedback Song, Chanho
 2001
 34 15 p. 493-498
6 p.
 artikel
72 Robust Flight Control Design With Eigenstructure Assignment Tokutake, Hiroshi
 2001
 34 15 p. 191-196
6 p.
 artikel
73 Robustness Analysis of a Launcher Attitude Controller Via µ-Analysis Imbert, Nicole
 2001
 34 15 p. 481-486
6 p.
 artikel
74 Robust Synthesis With Antiwindup Compensation for Electrohydraulic Servomechanism Ursu, Felicia
 2001
 34 15 p. 197-202
6 p.
 artikel
75 Satellite Autonomous Navigation Based on Image Motion Analysis Janschek, K.
 2001
 34 15 p. 111-116
6 p.
 artikel
76 Simultaneous Optimization of Intelligent Structure and Feedback Gains for Flexible Structure Control Li, Yong
 2001
 34 15 p. 536-541
6 p.
 artikel
77 Singular Extremals in Optimal Orbital Transfer Popescu, Mihai
 2001
 34 15 p. 173-178
6 p.
 artikel
78 Some Observations on Dynamics and Control of Spacecraft Formations Quadrelli, Marco B.
 2001
 34 15 p. 129-134
6 p.
 artikel
79 Some Questions of Safety And Efficiency Control of A Space Robotic Module's Flight Near by a Space Station Rutkovsky, V.Yu.
 2001
 34 15 p. 61-66
6 p.
 artikel
80 Spacecraft Attitude Determination Using Electrostatically Suspended Gyros Gusinsky, V.Z.
 2001
 34 15 p. 26-31
6 p.
 artikel
81 Space Robotics For Interplanetary Missions Schilling, K.
 2001
 34 15 p. 4-
1 p.
 artikel
82 Stability Theory Methods in Gyrostabilization Systems Dynamics Kuzmina, Lyudmila K.
 2001
 34 15 p. 117-122
6 p.
 artikel
83 Sub-Nanometric Optics Stabilization In View Of Gaia Astrometric Mission Canuto, Enrico
 2001
 34 15 p. 359-364
6 p.
 artikel
84 Suboptimal Guidance for Passive Homing Missile With Angle-Only-Measurement Lee, Ho-Il
 2001
 34 15 p. 443-448
6 p.
 artikel
85 Supervisioned Jet Thrusters and Piezoactuators Control for Vibration Suppression of a Large Flexible Structure Guarneri, D.
 2001
 34 15 p. 291-296
6 p.
 artikel
86 Synthesis of the Flexible Flight Control Algorithms Via Reflection Onto Integral Auxiliary Surfaces Pilishkin, V.N
 2001
 34 15 p. 167-172
6 p.
 artikel
87 The Effect of the Small Damping Sloshing to the Flexible Launch Vehicle Stability Suzuki, Hideto
 2001
 34 15 p. 185-190
6 p.
 artikel
88 The EFIGENIA EJ-1 An S/VTOL Autonomous Unmanned Aerial Vehicle Autocontrolled with an Adaptive Digital Reconfigurable Guidance, Navigation and Flight Control System Mario Andres Cordoba, G.
 2001
 34 15 p. 385-390
6 p.
 artikel
89 Transient Effects Related To Reconfigurable Control Design (Satellite Launcher) Ramos, F.O.
 2001
 34 15 p. 79-84
6 p.
 artikel
90 Waypoint-Based Fuzzy Guidance for Unmanned Aircraft Giulietti, Fabrizio
 2001
 34 15 p. 391-395
5 p.
 artikel
91 Wing-In-Ground Flight Automatic Control Principles, Systems and Application Advantages Nebylov, A.V.
 2001
 34 15 p. 542-547
6 p.
 artikel
                             91 gevonden resultaten
 
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