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                             99 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 Accurate and Stable Control of Shenzhou Spacecraft in Rendezvous and Docking * Xie, Yongchun
 2013
 46 19 p. 524-528
5 p.
 artikel
2 Adaptive Altitude Hold of a Small UAV with Switching Adaptation Laws Souanef, Toufik
 2013
 46 19 p. 212-217
6 p.
 artikel
3 Adaptive Sliding Mode Autopilot Design for Skid-To-Turn Missile Model with Uncertainties Ra, Chunggil
 2013
 46 19 p. 330-335
6 p.
 artikel
4 Advanced Autonomy for Low Cost Ground Stations Freimann, Andreas
 2013
 46 19 p. 388-392
5 p.
 artikel
5 Aerial Robot Localization Using Ground Robot Tracking – Towards Cooperative SLAM Nasir, Ahmad Kamal
 2013
 46 19 p. 313-318
6 p.
 artikel
6 Agile Attitude Control and Vibration Suppression of Flexible Spacecraft Using Control Moment Gyros Okubo, Hiroshi
 2013
 46 19 p. 417-422
6 p.
 artikel
7 Aircraft Nonlinear AFTC based on Geometric Approach and Singular Perturbations in case of actuator and sensor faults Castaldi, P.
 2013
 46 19 p. 30-35
6 p.
 artikel
8 An Autopilot Testbed for IMA (Integrated Modular Avionics) Architectures * Usach-Molina, H.
 2013
 46 19 p. 435-440
6 p.
 artikel
9 An EKF Based Generalized Estimation Approach for Evasive Targets Dwivedi, P.N.
 2013
 46 19 p. 307-312
6 p.
 artikel
10 A new attitude control design approach for flexible satellites Guy, Nicolas
 2013
 46 19 p. 500-505
6 p.
 artikel
11 Application of L1 Adaptive Controller to Longitudinal Dynamics of a High Manoeuvrability Aircraft Ene, Costin
 2013
 46 19 p. 447-452
6 p.
 artikel
12 Application of robust antiwindup design to the longitudinal aircraft control to cover actuator loss Guilhem, Puyou
 2013
 46 19 p. 506-511
6 p.
 artikel
13 Attitude Control and Momentum Management of Inertially Oriented Space Station Jun, ZHANG
 2013
 46 19 p. 1-6
6 p.
 artikel
14 Attitude Guidance and Control of Mini-satellites and Free-flying Robots * Rutkovsky, V.
 2013
 46 19 p. 399-404
6 p.
 artikel
15 Attitude & Orbit Digital and Pulse-width Control of Large-scale Communication Spacecraft * Somov, Ye.
 2013
 46 19 p. 376-381
6 p.
 artikel
16 Attitude stability analysis for an Earth pointing, magnetically controlled spacecraft Rossa, Fabio Delia
 2013
 46 19 p. 518-523
6 p.
 artikel
17 Bridging the gap between linear and nonlinear worst-case analysis: an application case to the atmospheric phase of the VEGA launcher Marcos, A.
 2013
 46 19 p. 42-47
6 p.
 artikel
18 Closed Loop Guidance Algorithm for Solid Propellant Rocket * Pietrobom, Hilton Cleber
 2013
 46 19 p. 31-36
6 p.
 artikel
19 Complex Flexible Aerospace Vehicles Simulation and Control System Design Panferov, Alexander I.
 2013
 46 19 p. 429-434
6 p.
 artikel
20 Conference Program 2013
 46 19 p. i-xxv
nvt p.
 artikel
21 Control design of ultra-quiet spacecraft platform Tang, Liang
 2013
 46 19 p. 266-270
5 p.
 artikel
22 Control of variable-pitch quadrotors Riccardi, Fabio
 2013
 46 19 p. 206-211
6 p.
 artikel
23 Cooperative guidance laws for maneuvering target interceptions Piet-Lahanier, H.
 2013
 46 19 p. 301-306
6 p.
 artikel
24 Cooperative guidance of UAVs for area exploration with final target allocation Gorecki, Tomasz
 2013
 46 19 p. 260-265
6 p.
 artikel
25 Coordinated Trajectory Planning for Efficient Communication Relay Using Multiple UAVs Oh, Hyondong
 2013
 46 19 p. 119-124
6 p.
 artikel
26 Differential Geometry based Collision Avoidance Guidance for Multiple UAVs Seo, Joongbo
 2013
 46 19 p. 113-118
6 p.
 artikel
27 Dynamic Programming Applications to Flight Trajectory Optimization Harada, Akinori
 2013
 46 19 p. 441-446
6 p.
 artikel
28 Dynamics Features and Algorithms of Gyroscopic Control of Large-Scale Flexible Spacecraft Rutkovsky, V.Yu.
 2013
 46 19 p. 364-369
6 p.
 artikel
29 Enhanced Linear Fractional Transformation: a Matlab Toolbox for Space System Modeling and Controller Analysis and Synthesis Kron, Aymeric
 2013
 46 19 p. 512-517
6 p.
 artikel
30 Estimating future aircraft intentions using short and long term behavior modeling Bisgaard, Morten
 2013
 46 19 p. 72-77
6 p.
 artikel
31 Evaluation and Performance Optimization of PMD Camera for RvD Application * Ravandoor, Karthik
 2013
 46 19 p. 149-154
6 p.
 artikel
32 Evolving Systems: Disturbance Accommodating Adaptive Key Component Control Balas, Mark J.
 2013
 46 19 p. 535-540
6 p.
 artikel
33 Experimental investigation of on-off control modulation for rigid and flexible free floating platforms Leonangeli, Nazareno
 2013
 46 19 p. 19-24
6 p.
 artikel
34 Fault Detection and Isolation for a Rocket Engine Valve Marcos, A.
 2013
 46 19 p. 101-106
6 p.
 artikel
35 Flat Stellar Dynamic Filter For Gyroless Attitude Estimation Pittet, C.
 2013
 46 19 p. 488-493
6 p.
 artikel
36 Flight Control of a Powered Paraglider by MIMO PID Control based on Two-Degree-of-Freedom Integral-type Optimal Servomechanism Ochi, Yoshimasa
 2013
 46 19 p. 188-193
6 p.
 artikel
37 Frequency and Time Domain Recursive Parameter Estimation For a Flexible Aircraft Majeed, M.
 2013
 46 19 p. 453-458
6 p.
 artikel
38 Funnel Flight Controller for a TDR 6-DoF Simulation Model Hopfe, Norman
 2013
 46 19 p. 125-130
6 p.
 artikel
39 Guidance and control for the propulsion phase of planetary landing Canuto, Enrico
 2013
 46 19 p. 370-375
6 p.
 artikel
40 Guidance of UAV EOLE for Launcher Separation Maneuver * Jouhaud, Frank
 2013
 46 19 p. 248-253
6 p.
 artikel
41 Hidden oscillations in stabilization system of flexible launcher with saturating actuators * Andrievsky, B.R.
 2013
 46 19 p. 37-41
5 p.
 artikel
42 H-Infinity control of the VEGA Launch Vehicle first stage in presence of roll Llana, David Sánchez de la
 2013
 46 19 p. 54-59
6 p.
 artikel
43 Hybrid System Identification for MIMO Control-System Design Bihl, Trevor J.
 2013
 46 19 p. 411-416
6 p.
 artikel
44 Identification of a Hammerstein model for an aerospace electrohydraulic servovalve Brito, Alexandro G.
 2013
 46 19 p. 459-463
5 p.
 artikel
45 Impacts of Space Plug-and-Play Technology on Micro- and Nano-satellites Kuwahara, T.
 2013
 46 19 p. 289-294
6 p.
 artikel
46 In-flight Calibration of Attitude Determination Systems for Information Mini-satellites * Somov, Ye.
 2013
 46 19 p. 393-398
6 p.
 artikel
47 Information Fusion Levels in Star Sensor Systems Strietzel, Roland
 2013
 46 19 p. 319-323
5 p.
 artikel
48 Innovative Fault Detection, Isolation and Recovery - Project Description Seidel, R.
 2013
 46 19 p. 96-100
5 p.
 artikel
49 Integrated Control and Structure design framework for spacecraft applied to Biomass satellite. Falcoz, Alexandre
 2013
 46 19 p. 13-18
6 p.
 artikel
50 Launch Vehicle Attitude Control System using PD plus Phase Lag Silva, A. G,
 2013
 46 19 p. 48-53
6 p.
 artikel
51 Longitudinal Flight Dynamics of a Single Tilt-wing Unmanned Aerial Vehicle Hong, Sungtae
 2013
 46 19 p. 60-65
6 p.
 artikel
52 Model-based Environment for Verification and Integration of Micro-satellites Kuwahara, T.
 2013
 46 19 p. 230-235
6 p.
 artikel
53 Model-Based On-Board Realtime Thruster Fault Monitoring Posch, A.
 2013
 46 19 p. 553-558
6 p.
 artikel
54 Modeling, Optimization, Simulation and Animation of Land-Survey Satellite Motion * Somov, S.Ye.
 2013
 46 19 p. 25-30
6 p.
 artikel
55 Model Predictive Control of Hayabusa2 Probe in the Approach Phase to an Asteroid Mimasu, Yuya
 2013
 46 19 p. 565-570
6 p.
 artikel
56 Modern Attitude Control and Co-design for the Biomass Satellite (Earth Explorer Core Mission 7) Massotti, Luca
 2013
 46 19 p. 405-410
6 p.
 artikel
57 Network-Centric Approach for Modular Avionics Herpel, H.-J.
 2013
 46 19 p. 178-182
5 p.
 artikel
58 New Advances of Chinese Spacecraft Control Technologies * Zhang, Duzhou
 2013
 46 19 p. 359-363
5 p.
 artikel
59 New Testing Facility for Proximity Operations in Space Regoli, Leonardo
 2013
 46 19 p. 353-358
6 p.
 artikel
60 Nonlinear Model Predictive Control of PEM Fuel Cell Systems for Generation of Exhaust Gas with Low Oxygen Content Schultze, M.
 2013
 46 19 p. 470-475
6 p.
 artikel
61 On Designing Fault Estimator for Satellite Attitude Control System with Typical Component Configuration Liu, Wengjing
 2013
 46 19 p. 107-112
6 p.
 artikel
62 On Grasping a Tumbling Debris Object with a Free-Flying Robot Lampariello, Roberto
 2013
 46 19 p. 161-166
6 p.
 artikel
63 On-line Collision Detection in Space Using Photonic Mixer Devices Scharnagl, Julian
 2013
 46 19 p. 143-148
6 p.
 artikel
64 Optimal Midcourse Guidance Law with Flight Path Angle and Lead Angle Constraints to Reach Circular Target Area Jeon, Byoung-Ju
 2013
 46 19 p. 336-340
5 p.
 artikel
65 Optimal Rendezvous Path Planning to an Uncontrolled Tumbling Target Michael, J.
 2013
 46 19 p. 347-352
6 p.
 artikel
66 Optimal Weapon Target Assignment Based on an Geometric Approach * Leboucher, C.
 2013
 46 19 p. 341-346
6 p.
 artikel
67 Parameter Identification Methods for Free-Floating Space Robots with direct Torque Sensing Rackl, Wolfgang
 2013
 46 19 p. 464-469
6 p.
 artikel
68 Particle Guidance: Applying POMDPs to the Optimization of Mid-Course Guidance Laws for Long-Range Missiles Pop-Stefanov, Bruno
 2013
 46 19 p. 295-300
6 p.
 artikel
69 Path Generation and Control for Unmanned Multirotor Vehicles Using Nonlinear Dynamic Inversion and Pseudo Control Hedging Raffler, Thomas
 2013
 46 19 p. 194-199
6 p.
 artikel
70 PICO-SATELLITE ORBIT AND ATTITUDE CONTROL BY ELECTRIC PROPULSION Kronhaus, Igal
 2013
 46 19 p. 277-282
6 p.
 artikel
71 Precision pointing estimator design for minimum absolute, window- and stability-time errors Graf, F.
 2013
 46 19 p. 224-229
6 p.
 artikel
72 Pulse-width Attitude Control of Large-scale Information Satellite at Service Modes * Somov, Sergey
 2013
 46 19 p. 7-12
6 p.
 artikel
73 Range extension of the PMD sensor with regard to applications in space * Tzschichholz, Tristan
 2013
 46 19 p. 324-329
6 p.
 artikel
74 Reactive Collision Avoidance of UAVs with Vision Sensing using Pin-hole Cameras Tripathi, Amit K.
 2013
 46 19 p. 66-71
6 p.
 artikel
75 Remote attitude control using delayed visual information - Nemo HD case study Klančar, Gregor
 2013
 46 19 p. 571-576
6 p.
 artikel
76 Rendezvous Simulation for On-Orbit Servicing Missions Using Advanced Robotic Technology Boge, T.
 2013
 46 19 p. 155-160
6 p.
 artikel
77 Return Strategies for Fixed-Wing MAVs After Loss of GPS Trittler, M.
 2013
 46 19 p. 254-259
6 p.
 artikel
78 Robust and Efficient OBDH Core Module for the Flexible Picosatellite Bus UWE-3 Busch, Stephan
 2013
 46 19 p. 218-223
6 p.
 artikel
79 Robust Satellite Engineering in Educational Cubesat Missions at the Example of the UWE-3 Project Busch, Stephan
 2013
 46 19 p. 236-241
6 p.
 artikel
80 Safe Approach Trajectory for Rendezvous1 Chen, Changqing
 2013
 46 19 p. 529-534
6 p.
 artikel
81 SAFE-V launcher validation framework and controller optimization Ganet-Schoeller, M.
 2013
 46 19 p. 482-487
6 p.
 artikel
82 Sampling-based path planning: a new tool for missile guidance Pharpatara, P.
 2013
 46 19 p. 131-136
6 p.
 artikel
83 SDS-4 Attitude Control System: In-Flight Results of Three Axis Attitude Control for Small Satellites Nakajima, Y.
 2013
 46 19 p. 283-288
6 p.
 artikel
84 Space based automatic identification and monitoring system for large-scale railway transportation – GP-AIMS * Kleinschrodt, A.
 2013
 46 19 p. 242-247
6 p.
 artikel
85 Spacecraft with Very High Pointing Stability: Experiences and Lessons Learned Yoshida, Norimasa
 2013
 46 19 p. 547-552
6 p.
 artikel
86 Stability analysis of pulse-modulated systems with an application to space launchers * Chaudenson, J.
 2013
 46 19 p. 494-499
6 p.
 artikel
87 Static input allocation for reaction wheels desaturation using magnetorquers Trégouët, Jean-François
 2013
 46 19 p. 559-564
6 p.
 artikel
88 Suboptimal Guidance of UAVs Satisfying Multiple Constraints on Waypoints Kumar, Prem
 2013
 46 19 p. 78-83
6 p.
 artikel
89 Sun tracking controller for UKube-1 using magnetic torquer only * Kim, Jongrae
 2013
 46 19 p. 541-546
6 p.
 artikel
90 System Identification of a Spacecraft Antenna Pointing Mechanism Kornienko, Andrei
 2013
 46 19 p. 172-177
6 p.
 artikel
91 Testing Satellite on-board Software - A Model Based Approach Zeuner, M.
 2013
 46 19 p. 167-171
5 p.
 artikel
92 The Attitude Determination and Control System of the Picosatellite UWE-3 * Reichel, F.
 2013
 46 19 p. 271-276
6 p.
 artikel
93 The Design, Ground Test and Flight Validation of a High Accuracy Servo Scheme for Control Moment Gyroscope Application Daning, Zhou
 2013
 46 19 p. 476-481
6 p.
 artikel
94 The Methods of Forecasting Some Events During the Aircraft Takeoff and Landing * Kuznetsov, A.
 2013
 46 19 p. 183-187
5 p.
 artikel
95 Three-dimensional Impact Angle Control Guidance Law for Missiles Using Dual Sliding Surfaces Lee, Yongwoo
 2013
 46 19 p. 137-142
6 p.
 artikel
96 VAMOS – Verification of Autonomous Mission Planning On-board a Spacecraft Wille, Benjamin
 2013
 46 19 p. 382-387
6 p.
 artikel
97 Verification and validation of a FDD system for identification of aircraft control surface jamming * Varga, A.
 2013
 46 19 p. 84-89
6 p.
 artikel
98 VIMOS - Autonomous image analysis on board of BIROS Goetz, Katharina A.M.
 2013
 46 19 p. 423-428
6 p.
 artikel
99 Visual Servoing Based Landing Approach Controller for Fixed-Wing MAVs Trittler, M.
 2013
 46 19 p. 200-205
6 p.
 artikel
                             99 gevonden resultaten
 
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