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                             153 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 ACCELERO-STELLAR HYBRIDIZATION FOR MICROSCOPE DRAG FREE MISSION Pittet, C.
 2007
 40 7 p. 271-276
6 p.
 artikel
2 A CONVEX APPROACH TO THE DESIGN OF OPTIMAL TRAJECTORIES FOR SATELLITE Louembet, Christophe
 2007
 40 7 p. 153-158
6 p.
 artikel
3 ADAPTIVE PASSIFICATION-BASED FAULT-TOLERANT FLIGHT CONTROL Fradkov, Alexander L.
 2007
 40 7 p. 715-720
6 p.
 artikel
4 AEROSPACE GAIN SCHEDULING DESIGN USING GENETIC OPTIMISATION Britto, Alexandro Garro
 2007
 40 7 p. 792-797
6 p.
 artikel
5 A FAULT TOLERANT CONTROL SUPERVISORY SYSTEM DEVELOPMENT PROCEDURE FOR SMALL SATELLITES - THE AAUSAT-II CASE Izadi-Zamanabadi, Roozbeh
 2007
 40 7 p. 289-294
6 p.
 artikel
6 A GENETIC APPROACH TO ANTI-AIR MISSILE CONTROL SYSTEM DESIGN Mehrabian, Ali Reza
 2007
 40 7 p. 61-66
6 p.
 artikel
7 A GRAVITATIONAL REFERENCE SENSOR FOR ADVANCED DRAG-FREE SATELLITES Allen, Graham
 2007
 40 7 p. 277-282
6 p.
 artikel
8 A GUIDANCE LAW WITH SINUSOIDAL EVASIVE MANEUVER FOR ENHANCING SURVIVABILITY OF ANTI-SHIP MISSILES Lee, Jin-Ik
 2007
 40 7 p. 804-809
6 p.
 artikel
9 A HYBRID ENERGY-INSENSITIVE EXPLICIT GUIDANCE SCHEME FOR LONG RANGE FLIGHT VEHICLES WITH SOLID MOTORS Kothari, Mangal
 2007
 40 7 p. 651-656
6 p.
 artikel
10 AIRCRAFT AIR DATA ESTIMATION USING A MODEL-BASED APPROACH Pearson, J.T.
 2007
 40 7 p. 557-562
6 p.
 artikel
11 AIRCRAFT GUIDANCE LAW WITH TRAJECTORY CONSTRAINTS Geri, Walter
 2007
 40 7 p. 527-532
6 p.
 artikel
12 AN ADAPTIVE TAKAGI-SUGENO FUZZY GUIDANCE LAW WITH HIGH GAIN OBSERVER CONSIDERING MISSILE UNCERTAINTIES AND TARGET MANOEUVRE Abedi, Mostafa
 2007
 40 7 p. 55-60
6 p.
 artikel
13 AN ATTITUDE CONTROL STRATEGY FOR SPINNING SOLAR SAIL Tsuda, Yuichi
 2007
 40 7 p. 401-406
6 p.
 artikel
14 AN EXPERIMENTAL STUDY ON ATTITUDE CONTOL OF SPACECRAFT USING FUZZY CONTROLLER Park, Jong-Oh
 2007
 40 7 p. 491-496
6 p.
 artikel
15 A NOVEL METHOD FOR FLIGHT CONTROL LAWS ROBUSTNESS ANALYSIS OVER UNSTEADY TRAJECTORIES Tancredi, U.
 2007
 40 7 p. 347-352
6 p.
 artikel
16 AN UNDERGRADUATE-STUDENT AUTONOMOUS VIDEO-SURVEILANCE UAV PROJECT Schmidt, David K.
 2007
 40 7 p. 726-731
6 p.
 artikel
17 A PD+ APPROACH TO 6DOF SPACECRAFT COORDINATION CONTROL Kristiansen, Raymond
 2007
 40 7 p. 241-246
6 p.
 artikel
18 APPROXIMATE NONLINEAR OPTIMAL SDRE TRACKING CONTROL çimen, Tayfun
 2007
 40 7 p. 147-152
6 p.
 artikel
19 A ROBUST CONTROLLER STRUCTURE FOR PICO-SATELLITE APPLICATIONS Green, Martin
 2007
 40 7 p. 738-743
6 p.
 artikel
20 A380 ROLL KINEMATICS DESIGN DELANNOY, Stéphane
 2007
 40 7 p. 103-108
6 p.
 artikel
21 A SMART APPROACH TO PRECISION ATTITUDE MANEUVERS OF SPACECRAFTS Chunodkar, Apurva
 2007
 40 7 p. 141-146
6 p.
 artikel
22 ASYMPTOTICALLY OPTIMAL NONLINEAR FILTERING çimen, Tayfun
 2007
 40 7 p. 756-761
6 p.
 artikel
23 ATMOSPHERIC RE-ENTRY NDI CONTROL DESIGN FOR THE HOPPER RLV CONCEPT Marcos, Andrés
 2007
 40 7 p. 786-791
6 p.
 artikel
24 ATTITUDE CONTROL OF SPACECRAFT WITH PARTIALLY MAGNETIC ACTUATION Pulecchi, Tiziano
 2007
 40 7 p. 609-614
6 p.
 artikel
25 ATTITUDE & ORBIT CONTROL SYSTEM FOR GALILEO IOV * Konrad, Alexej
 2007
 40 7 p. 25-30
6 p.
 artikel
26 Author Index 2007
 40 7 p. 25-29
5 p.
 artikel
27 AUTOMATIC AERIAL REFUELING FOR CCV VIA LOS-ANGLE AND RANGE CONTROL Ochi, Yoshimasa
 2007
 40 7 p. 73-78
6 p.
 artikel
28 Autonomous Intelligent Fuzzy Logic Guidance, and Flight Control System for the EFIGENIA EJ-1B MOZART Unmanned Aerial Vehicle UAV Cordoba, G. Mario Andres
 2007
 40 7 p. 31-36
6 p.
 artikel
29 CAREFREE MANOEUVRING AND AUTOMATIC RETURN TO NORMAL FLIGHT ENVELOPE JAS 39 GRIPEN. SAAB AB, Robert Hillgren
 2007
 40 7 p. 115-120
6 p.
 artikel
30 COMBINED FLIGHT GUIDANCE OPTIMIZATION BY GENETIC PROGRAMMING AND SIMPLEX METHOD Takano, Hiroyuki
 2007
 40 7 p. 865-870
6 p.
 artikel
31 COMMAND TRACKING IN HIGH PERFORMANCE AIRCRAFTS: A NEW DYNAMIC INVERSION DESIGN Padhi, R.
 2007
 40 7 p. 79-84
6 p.
 artikel
32 COMPARATIVE ANALYSIS OF DESIGN VARIANTS FOR LOW ALTITUDE FLIGHT PARAMETERS MEASURING SYSTEM Nebylov, Alexander
 2007
 40 7 p. 663-668
6 p.
 artikel
33 CONCEPT FOR THE DESIGN OF FLIGHT CONTROL ACTUATION AND LAWS FOR FUTURE ALL-ELECTRIC AIRCRAFT Schallert, Christian
 2007
 40 7 p. 67-72
6 p.
 artikel
34 CONTRACTIVE MODEL PREDICTIVE CONTROL OF AN UNMANNED AERIAL VEHICLE MODEL Bertrand, Sylvain
 2007
 40 7 p. 450-455
6 p.
 artikel
35 CONTROL OF A FLEXIBLE ROBOT WITH FUZZY LOGIC AND A NONCOLLOCATED SENSOR LOCATION Sasiadek, A. Green J.Z.
 2007
 40 7 p. 877-882
6 p.
 artikel
36 CONTROL OF MARS GUIDED ENTRY (PART II): ROBUST NONLINEAR DYNAMICS INVERSION Kron, Aymeric
 2007
 40 7 p. 581-586
6 p.
 artikel
37 CONTROL OF MARS GUIDED ENTRY (PART I): ROBUST SELF-SCHEDULING MODAL CONTROL Torralba, José
 2007
 40 7 p. 575-580
6 p.
 artikel
38 COOPERATIVE ATTITUDE SYNCHRONIZATION IN SATELLITE SWARMS: A CONSENSUS APPROACH Sarlette, Alain
 2007
 40 7 p. 223-228
6 p.
 artikel
39 COUPLED LPV AND FLATNESS BASED APPROACH FOR LOW LIFT RE-ENTRY VEHICULE GUIDANCE Zerar, Madjid
 2007
 40 7 p. 189-194
6 p.
 artikel
40 DESIGN AND IMPLEMENTATION OF AN ADAPTIVE PI CONTROLLER FOR A TWO AXIS GIMBAL SYSTEM Golmohammad, Hassan
 2007
 40 7 p. 889-894
6 p.
 artikel
41 DESIGN AND PERFORMANCE ANALYSIS OF RESIDUAL GENERATORS FOR THE FDI OF AIRCRAFT MODEL SENSORS Simani, S.
 2007
 40 7 p. 91-96
6 p.
 artikel
42 DESIGN OF AN AGC DRIVING LOOP IN MEMS GYROSCOPES Sung, Woon-Tahk
 2007
 40 7 p. 335-340
6 p.
 artikel
43 DEVELOPMENT OF AN ON-BOARD FAULT TOLERANT CONTROL STRATEGY WITH APPLICATION TO THE GARTEUR AG16 BENCHMARK Cieslak, J.
 2007
 40 7 p. 97-102
6 p.
 artikel
44 DEVELOPMENT OF AUTOMATIC FLIGHT CONTROL SYSTEMS FOR WING IN SURFACE EFFECT CRAFT Muhammad, Hari
 2007
 40 7 p. 109-114
6 p.
 artikel
45 3D TRAJECTORY TRACKING FOR A FIXED WING UNMANNED AERIAL VEHICLE USING DYNAMIC INVERSION Boukraa, D.
 2007
 40 7 p. 443-449
7 p.
 artikel
46 DYNAMICS AND CONTROL OF FLEXIBLE SPACE STRUCTURES DURING THEIR ASSEMBLY IN AN ORBIT Rutkovsky, V.Yu.
 2007
 40 7 p. 365-370
6 p.
 artikel
47 EARTH ORIENTED SAFE MODE DESIGN BASED ON THE EADS ASTRIUM CESS Levenhagen, J.
 2007
 40 7 p. 301-304
4 p.
 artikel
48 ELECTROSTATIC ACCELEROMETER AS AN ADVANTAGEOUS COMPONENT OF PRECISE ATTITUDE AND ORBIT CONTROL SYSTEM Gomez, A.
 2007
 40 7 p. 259-264
6 p.
 artikel
49 Evaluation of ground and orbit microvibration of OICETS OOI, Yoshitaka
 2007
 40 7 p. 265-270
6 p.
 artikel
50 EXTENDING THE LINEAR QUADRATIC DESIGN OF A LAUNCH VEHICLE ATTITUDE CONTROLLER THROUGH GENETIC OPTIMIZATION Ramos, Fausto O.
 2007
 40 7 p. 780-785
6 p.
 artikel
51 FAULT TOLERANT FLIGHT CONTROL SYSTEM BASED ON FUZZY-TUNING IMM FILTER Kim, Seungkeun
 2007
 40 7 p. 675-680
6 p.
 artikel
52 FEEDFORWARD UNSCENTED KALMAN FILTER FOR INS/GPS TIGHTLY COUPLED INTEGRATION SYSTEM Kim, Kwangjin
 2007
 40 7 p. 545-550
6 p.
 artikel
53 FLIGHT MODEL IDENTIFICATION OF AN F/A-18 FROM FLIGHT TESTS Beaulieu, M. Nadeau
 2007
 40 7 p. 212-216
5 p.
 artikel
54 FLIGHT TEST OF IN-FLIGHT SIMULATOR CONTROLLER FOR SIMULTANEOUS SIMULATION OF GUST RESPONSE AND HANDLING RESPONSE Sato, Masayuki
 2007
 40 7 p. 853-858
6 p.
 artikel
55 FLYING QUALITIES OF RE-ENTRY VEHICLE WORST CASE ANALYSIS AND INERTIAL ROLL COUPLING GANET-SCHOELLER, Martine
 2007
 40 7 p. 603-608
6 p.
 artikel
56 FORMATION FLYING NAVIGATION AND CONTROL PROBLEMATICS AND APPLICATIONS Guidotti, Pierre-Yves
 2007
 40 7 p. 229-234
6 p.
 artikel
57 FREE-FLYING SPACE ROBOTIC MODULE: ADAPTIVE COMPUTER AIDED PRECIZE CONTROL Zemlyakov, S.D.
 2007
 40 7 p. 521-526
6 p.
 artikel
58 Front Cover 2007
 40 7 p. i-
1 p.
 artikel
59 FULL-MATRIX INVERSE-BASED MIMO QFT CONTROL DESIGN FOR SPACECRAFT FLYING IN FORMATION Garcia-Sanz, M.
 2007
 40 7 p. 165-170
6 p.
 artikel
60 GAIN-SCHEDULED FLIGHT CONTROL LAW FOR FLEXIBLE AIRCRAFT: A PRACTICAL APPROACH Puyou, Guilhem
 2007
 40 7 p. 497-502
6 p.
 artikel
61 GAIN SCHEDULING CONTROLLER DESIGN FOR ENGINEERING TEST SATELLITE-VIII Hamada, Yoshiro
 2007
 40 7 p. 591-596
6 p.
 artikel
62 GENERIC 4D FLIGHT GUIDANCE BASED ON DIFFERENTIAL FLATNESS Lu, Wen Chi
 2007
 40 7 p. 353-358
6 p.
 artikel
63 GENETIC ALGORITHM FOR COUPLED RLV TRAJECTORY AND GUIDANCE OPTIMIZATION VERNIS, Philippe
 2007
 40 7 p. 569-574
6 p.
 artikel
64 GNC FOR THE PEGASE MISSION Villien, Anthony
 2007
 40 7 p. 389-394
6 p.
 artikel
65 GUIDANCE AND ATTITUDE CONTROL LAW FOR THE FINAL PART OF A REENTRY VEHICLE TRAJECTORY - ALTERNATE LAWS FOR THE EXPERIMENTAL VEHICLE HSFD II * Jouhaud, Frank
 2007
 40 7 p. 311-316
6 p.
 artikel
66 GUIDANCE AND CONTROL SYSTEM FOR POINTING-DEVICE-CONTROLLED AIRCRAFT Yamasaki, Takeshi
 2007
 40 7 p. 85-90
6 p.
 artikel
67 GUIDANCE AND ROBUST GYROMOMENT ATTITUDE CONTROL OF AGILE FLEXIBLE REMOTE SENSING SPACECRAFT Somov, Ye.
 2007
 40 7 p. 533-538
6 p.
 artikel
68 HIGH POINTING ACCURACY WITH THE PICARD MICRO SATELLITE. Samson, P.
 2007
 40 7 p. 295-300
6 p.
 artikel
69 HIGH-POWERED NON-LINEAR SHOCK DAMPER USING ER FLUID Makihara, Kanjuro
 2007
 40 7 p. 597-602
6 p.
 artikel
70 HYBRID DAMAGE ADAPTIVE FLIGHT CONTROL WITH MODEL INVERSION ADAPTATION Nguyen, Nhan
 2007
 40 7 p. 657-662
6 p.
 artikel
71 HYBRID INVERSE METHODS FOR HELICOPTERS IN AGGRESSIVE MANOEUVRING FLIGHT Bagiev, Marat
 2007
 40 7 p. 419-424
6 p.
 artikel
72 ICC2 STUDY: GNC DEVELOPMENT IN FORMATION FLYING Pirson, L.
 2007
 40 7 p. 828-833
6 p.
 artikel
73 IMPROVED DELTA METHOD FOR PARAMETER ESTIMATION FROM REAL-FLIGHT DATA USING NEURAL NETWORKS Singh, S.
 2007
 40 7 p. 200-205
6 p.
 artikel
74 IN-FLIGHT IDENTIFICATION OF THE AUGMENTED FLIGHT DYNAMICS OF THE RMAX UNMANNED HELICOPTER Duranti, Simone
 2007
 40 7 p. 217-222
6 p.
 artikel
75 INS AIDING USING BEARINGS-ONLY MEASUREMENTS OF KNOWN GROUND OBJECTS Pachter, M.
 2007
 40 7 p. 539-544
6 p.
 artikel
76 INTEGRATION OF H ∞ AND TIME DOMAIN SPECIFICATIONS USING THE CONVEX COMBINATION METHOD Ahmed, Shakil
 2007
 40 7 p. 135-140
6 p.
 artikel
77 INTERVAL BISECTION METHOD FOR CONTROL ALLOCATION Demenkov, Max
 2007
 40 7 p. 183-188
6 p.
 artikel
78 LARGE “FUROSHIKI” NET EXTENSION IN SPACE – SOUNDING ROCKET EXPERIMENT RESULTS Nakasuka, Shinichi
 2007
 40 7 p. 485-490
6 p.
 artikel
79 LATERAL CONTROL WITH IMPROVED PERFORMANCE FOR UAVs Samar, R.
 2007
 40 7 p. 37-42
6 p.
 artikel
80 LEO MYRIADE AOCS ADAPTION TO GTO FOR SPIRALE MISSION Montfort, E.
 2007
 40 7 p. 615-620
6 p.
 artikel
81 LINKMAV, A PROTOYPE ROTARY WING MICRO AERIAL VEHICLE Duranti, S.
 2007
 40 7 p. 473-478
6 p.
 artikel
82 LMI CONSTRAINT FOR PHASE CONTROL OF BENDING MODES: APPLICATION TO THE ATTITUDE CONTROL OF A SATELLITE ABBAS-TURKI, Mohamed
 2007
 40 7 p. 341-346
6 p.
 artikel
83 LOCAL ORBITAL FRAME OBSERVER FOR LEO DRAG-FREE SATELLITES Canuto, Enrico S.
 2007
 40 7 p. 840-845
6 p.
 artikel
84 LONGITUDINAL ROBUST ANISOTROPIC OPTIMAL FLIGHT CONTROL IN A WINDSHEAR Kurdyukov, A.P.
 2007
 40 7 p. 822-827
6 p.
 artikel
85 LONGITUDINAL STABILITY AND CONTROL OF LARGE TILT-ROTOR AIRCRAFT Walker, D.J.
 2007
 40 7 p. 413-418
6 p.
 artikel
86 LYAPUNOV BASED STABILITY ANALYSIS OF A THREE-TIME SCALE MODEL FOR A HELICOPTER ON A PLATFORM 1 Esteban, Sergio
 2007
 40 7 p. 467-472
6 p.
 artikel
87 MISSILE AUTOPILOT DESIGN USING OBSERVER-BASED GAIN SCHEDULING Theodoulis, Spilios
 2007
 40 7 p. 798-803
6 p.
 artikel
88 MODEL-BASED SOLUTIONS FOR STRUCTURAL COUPLING PROBLEMS IN AIRCRAFT Halsey, S.A.
 2007
 40 7 p. 503-508
6 p.
 artikel
89 MODELLING AND PERFORMANCE ANALYSIS OF INTEGRATED AVIONICS BUS SYSTEM JianDong, Zhang
 2007
 40 7 p. 687-691
5 p.
 artikel
90 MODE-SHAPES CORRELATION AND CUSUM TEST FOR ON-LINE FLUTTER MONITORING Zouari, Rafik
 2007
 40 7 p. 206-211
6 p.
 artikel
91 MORPHABLE BEAM DEVICE AND ITS VISUAL POSITIONING SYSTEM Iljic, Thomas
 2007
 40 7 p. 871-876
6 p.
 artikel
92 MULTI CLASSIFIER FUSION TO AIR TARGET CLASSIFICATOIN Golmohammad, Hassan
 2007
 40 7 p. 744-749
6 p.
 artikel
93 MULTIRATE & NONLINEAR CONTROLLERS FOR LOW-COST LASER TRACKING SYSTEMS Anderson, David
 2007
 40 7 p. 816-821
6 p.
 artikel
94 NANO-SATELLITE ATTITUDE STABILIZATION METHOD USING STAR IMAGES Sako, Nobutada
 2007
 40 7 p. 587-590
4 p.
 artikel
95 NONLINEAR ACTUATOR FAULT DETECTION AND ISOLATION FOR A GENERAL AVIATION AIRCRAFT Castaldi, P.
 2007
 40 7 p. 709-714
6 p.
 artikel
96 NONLINEAR RECONFIGURABLE FLIGHT CONTROL SYSTEM USING MULTIPLE MODEL ADAPTIVE CONTROL Jung, Bokyung
 2007
 40 7 p. 171-176
6 p.
 artikel
97 NONLINEAR RE-ENTRY FLIGHT CONTROL SYSTEM ROBUSTNESS EVALUATION USING INTERVAL ANALYSIS Juliana, Sinar
 2007
 40 7 p. 329-334
6 p.
 artikel
98 NONLINEAR ROBUST MODEL PREDICTIVE CONTROL FOR LIFTING BODY RE-ENTRY FLIGHT ATTITUDE CONTROL van Oort, E.R.
 2007
 40 7 p. 323-328
6 p.
 artikel
99 OFF LINE DIAGNOSIS OF ARIANE FLIGHTS USING PCA Barta, César
 2007
 40 7 p. 704-708
5 p.
 artikel
100 ON THE DESIGN OF A FLATNESS-BASED GUIDANCE ALGORITHM FOR THE TERMINAL AREA ENERGY MANAGEMENT OF A WINGED-BODY VEHICLE Morio, Vincent
 2007
 40 7 p. 563-568
6 p.
 artikel
101 OPTIMAL ATTITUDE CONTROL THROUGH MAGNETIC TORQUERS AND REACTION WHEELS Tewari, Ashish
 2007
 40 7 p. 19-24
6 p.
 artikel
102 OPTIMAL AVERAGE CONSENSUS ON MULTI-AGENT NETWORKS 1 Kim, Yoonsoo
 2007
 40 7 p. 235-240
6 p.
 artikel
103 OPTIMAL ORBIT CONTROL OF SPACECRAFT ON ELLIPTICAL ORBITS Vigano, Luca
 2007
 40 7 p. 13-18
6 p.
 artikel
104 OSCILLATORY FAILURE CASE DETECTION IN THE A380 ELECTRICAL FLIGHT CONTROL SYSTEM BY ANALYTICAL REDUNDANCY. Goupil, P.
 2007
 40 7 p. 681-686
6 p.
 artikel
105 PARSIMONIOUS MODEL FOR AIR-DATA READOUT FROM “ON-SKIN” PRESSURE MEASUREMENTS IN SUBSONIC FLOWS Callegari, Sergio
 2007
 40 7 p. 253-258
6 p.
 artikel
106 PATH PLANNING OF MULTIPLE UAVS WITH CLOTHOID CURVES IN TWO DIMENSIONS Shanmugavel, Madhavan
 2007
 40 7 p. 461-466
6 p.
 artikel
107 PERFORMANCE EVALUATION OF KALMAN FILTER FOR FAULT DETECTION OF HYDRAULIC ACTUATORS Muenchhof, Marco
 2007
 40 7 p. 692-697
6 p.
 artikel
108 PLANETARY ROVER MOBILITY: WHEEL-SOIL INTERACTION BASED ON MULTIBODY SYSTEM APPROACH Schäfer, Bernd
 2007
 40 7 p. 883-888
6 p.
 artikel
109 PLEIADES-HR CMGs-BASED ATTITUDE CONTROL SYSTEM DESIGN, DEVELOPMENT STATUS AND PERFORMANCES Thieuw, Alain
 2007
 40 7 p. 834-839
6 p.
 artikel
110 POLYNOMIAL LPV SYNTHESIS APPLIED TO TURBOFAN ENGINES Gilbert, Wilfried
 2007
 40 7 p. 645-650
6 p.
 artikel
111 PREDICTION OF HELICOPTER CRITICAL FLIGHT REGIMEN BY CONTINUATION AND BIFURCATION METHODS Sibilski, Krzysztof
 2007
 40 7 p. 437-442
6 p.
 artikel
112 Preshaping Profiler for Flexible Spacecraft Rest-to-Rest Maneuvers Kamiya, Toshio
 2007
 40 7 p. 283-288
6 p.
 artikel
113 PROGRAMME 2007
 40 7 p. 7-23
17 p.
 artikel
114 QUASI-OPTIMUM CONTROL AND THE SDRE METHOD Friedland, Bernard
 2007
 40 7 p. 762-767
6 p.
 artikel
115 RADOME COMPENSATION USING ADAPTIVE PARTICLE FILTER Han, Sang Sul
 2007
 40 7 p. 43-48
6 p.
 artikel
116 REAL-TIME AUTOMATIC TUNING OF AN AIRCRAFT SIDESLIP ESTIMATOR Ronceray, Lilian
 2007
 40 7 p. 859-864
6 p.
 artikel
117 RELATIVE MOTION ESTIMATION AND CONTROL TO A FAILED SATELLITE BY MACHINE VISION Terui, Fuyuto
 2007
 40 7 p. 639-644
6 p.
 artikel
118 RESILIENT STRUCTURED PERIODIC H 2 SYNTHESIS FOR A SPACECRAFT IN ELLIPTICAL ORBITS Farges, C.
 2007
 40 7 p. 633-638
6 p.
 artikel
119 ROBUST AIRCRAFT CONTROL DESIGN WITH REDUCED STABILITY AND SATURATED ACTUATORS Feuersänger, Alexander P.
 2007
 40 7 p. 621-626
6 p.
 artikel
120 ROBUST ATTITUDE CONTROL OF ETS-VIII SPACECRAFT VIA SYMMETRIC CONTROLLER Nagashio, Tomoyuki
 2007
 40 7 p. 7-12
6 p.
 artikel
121 ROBUST FDI APPLIED TO THRUSTER FAULTS OF A SATELLITE SYSTEM Patton, Ron J.
 2007
 40 7 p. 1-6
6 p.
 artikel
122 ROBUST FLATNESS BASED CONTROL AND MOTION PLANNING OF A MUAV Rontani, Damien
 2007
 40 7 p. 359-364
6 p.
 artikel
123 ROBUST GYROMOMENT SPACECRAFT ATTITUDE CONTROL WITH PRECISE POINTING A FLEXIBLE ANTENNA Somov, Ye.
 2007
 40 7 p. 515-520
6 p.
 artikel
124 ROLL ANGLE ESTIMATION FOR SMART MUNITIONS Park, HeeYoung
 2007
 40 7 p. 49-54
6 p.
 artikel
125 ROSETTA AOCS BEHAVIOUR IN THE FIRST YEARS OF OPERATIONS Reuilh, Anne
 2007
 40 7 p. 383-388
6 p.
 artikel
126 SDRE AUTOPILOT FOR DUAL CONTROLLED MISSILES Mracek, Curtis P.
 2007
 40 7 p. 750-755
6 p.
 artikel
127 SDRE CONTROL OF THE CONTROL ACTUATION SYSTEM OF A GUIDED MISSILE Merttopçuoğlu, A.O.
 2007
 40 7 p. 774-779
6 p.
 artikel
128 SDRE MISSILE AUTOPILOT DESIGN USING SLIDING MODE CONTROL WITH MOVING SLIDING SURFACES Salamci, Metin U.
 2007
 40 7 p. 768-773
6 p.
 artikel
129 SEA PLANE LANDING CONTROL AT WAVE DISTURBANCES Nebylov, A.V.
 2007
 40 7 p. 669-674
6 p.
 artikel
130 SENSOR AND CONTROL SURFACE/ACTUATOR FAILURE DETECTION BASED ON THE SPECTRAL NORM OF AN INNOVATION MATRIX Hajiyev, Chingiz
 2007
 40 7 p. 698-703
6 p.
 artikel
131 SIMULATION AND CONTROL OF FLEXIBLE VEHICLES Brodsky, S.A.
 2007
 40 7 p. 371-376
6 p.
 artikel
132 SINGULARITY AVOIDANCE LAW FOR CMG USING VIRTUAL ACTUATOR Lee, Hyunjae
 2007
 40 7 p. 305-310
6 p.
 artikel
133 SLIDING MODE TECHNIQUE APPLIED TO TEST MASS SUSPENSION CONTROL Montemurro, Fabio
 2007
 40 7 p. 627-632
6 p.
 artikel
134 SPACECRAFT COORDINATION CONTROL USING PID+ BACKSTEPPING Kristiansen, Raymond
 2007
 40 7 p. 247-252
6 p.
 artikel
135 SPACECRAFT LOCALIZATION VIA ANGLE MEASUREMENTS FOR AUTONOMOUS NAVIGATION IN DEEP SPACE MISSIONS Ceccarelli, Nicola
 2007
 40 7 p. 551-556
6 p.
 artikel
136 STABILITY AND PERFORMANCE ENHANCEMENT OF A FIGHTER AIRCRAFT FLIGHT CONTROL SYSTEM BY A NEW ANTI-WINDUP APPROACH Biannic, Jean-Marc
 2007
 40 7 p. 177-182
6 p.
 artikel
137 STABILITY INHERITANCE AND CONTACT DYNAMICS OF FLEXIBLE STRUCTURE EVOLVING SYSTEMS Frost, Susan A.
 2007
 40 7 p. 479-484
6 p.
 artikel
138 STABILIZATION OF UNDERACTUATED SPACECRAFT DYNAMICS VIA SINGULARLY PERTURBED FEEDBACK LINEARIZATION Bajodah, Abdulrahman H.
 2007
 40 7 p. 377-382
6 p.
 artikel
139 STATE ESTIMATION OVER THE LIMITED-BAND COMMUNICATION CHANNEL FOR PITCH MOTION CONTROL OF LAAS HELICOPTER BENCHMARK 1 Andrievsky, Boris
 2007
 40 7 p. 407-412
6 p.
 artikel
140 Stepping Motor Driving Disturbance Test and Identification of Mathematical Disturbance Model Kamiya, Toshio
 2007
 40 7 p. 509-514
6 p.
 artikel
141 SYSTEM DESIGN OF THE BARRACUDA FLIGHT CONTROL SYSTEM Schönhoff, A.
 2007
 40 7 p. 121-128
8 p.
 artikel
142 THE BARRACUDA AUTOFLIGHT MODULE FOR AUTONOMOUS FLIGHT Moormann, D.
 2007
 40 7 p. 846-851
6 p.
 artikel
143 THE DECENTRALIZED NONLINEAR MODEL PREDICTIVE FORMATION FLIGHT Shin, J. Ho
 2007
 40 7 p. 159-164
6 p.
 artikel
144 THE DEVELOPMENT OF FLIGHT CONTROL SYSTEM FOR THE CLOSE RANGE SURVEILLANCE UAV Choi, Seung-Kie
 2007
 40 7 p. 456-460
5 p.
 artikel
145 THE PICO-SATELLITE UWE-1 AND IP BASED TELECOMMUNICATION EXPERIMENTS Schmidt, Marco
 2007
 40 7 p. 721-725
5 p.
 artikel
146 THE SPECIFIC FEATURES OF FBW CONTROL LAWS OF ADVANCED REGIONAL JET Didenko, Yury
 2007
 40 7 p. 129-134
6 p.
 artikel
147 TOKYO TECH NANO-SATELLITE CUTE-1.7 + APD FLIGHT OPERATION RESULTS AND THE SUCCEEDING SATELLITE Fujiwara, Ken
 2007
 40 7 p. 732-737
6 p.
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148 TRAJECTORY TRACKING H 2 CONTROLLER FOR AUTONOMOUS HELICOPTERS: AN APPLICATION TO INDUSTRIAL CHIMNEY INSPECTION Guerreiro, B.
 2007
 40 7 p. 431-436
6 p.
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149 VERIFICATION METHOD FOR EMBEDDED REAL TIME SYSTEMS OF AEROSPACE APPLICATION Nebylov, A.V.
 2007
 40 7 p. 195-199
5 p.
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150 VISION AIDED STATE ESTIMATOR FOR HELICOPTER SLUNG LOAD SYSTEM Bisgaard, Morten
 2007
 40 7 p. 425-430
6 p.
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151 VISION NAVIGATION FOR EUROPEAN LANDERS AND THE NPAL PROJECT Bodineau, G.
 2007
 40 7 p. 395-400
6 p.
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152 WORST-CASE ANALYSIS OF FLIGHT CONTROL LAWS FOR RE-ENTRY VEHICLES Menon, P.P.
 2007
 40 7 p. 317-322
6 p.
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153 ZERO-SUM VERSUS NONZERO-SUM DIFFERENTIAL GAME APPROACH TO MISSILE GUIDANCE Trottemant, E.J.
 2007
 40 7 p. 810-815
6 p.
 artikel
                             153 gevonden resultaten
 
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