About 192 item dissertation in line with V448.22,Attitude Control System query results,the following is 1 to 50(Search took 0.021 seconds)

  1. Research on Novel Approach for Gyroless Angular Rate Measurement Based on Star Tracker,LiuHaiBo/National University of Defense Science and Technology,0/116
  2. Study on the Drive and Control System of the Reaction Flywheel,ZhangPing/Harbin Institute of Technology,0/36
  3. Research on Fault Tolerant Control of Satellite Attitude System,YangZuo/Harbin Institute of Technology,0/35
  4. Research on Small Satellite Attitude Control by Fluid Momentum Loops,DanXiaoWei/Harbin Institute of Technology,0/25
  5. Research on Satellite Attitude Control Based on Data-driven Theory,WangDongWei/Harbin Institute of Technology,0/23
  6. Model-based Fault Diagnosis for Satellite Attitude Control System,ChengYao/Harbin Institute of Technology,0/38
  7. Quaternion-based Space Interceptor Attitude Control Design,ZhaoQin/Harbin Institute of Technology,0/63
  8. The Research on the Control Algorithms of Large-angle Maneuver of Small Wheel-controlled Satellite,ZhangCheng/Harbin Institute of Technology,0/17
  9. The Implementation of the Drive and Control of Variable Speed Flywheel System,XuChunLei/Harbin Institute of Technology,0/31
  10. Design and Verification of Data Collection Module of Sun-sensor SoC,MengChao/Harbin Institute of Technology,0/9
  11. Design and Verification on Sun Sensor Threshold Centroid Algorithm,ZhaoChen/Harbin Institute of Technology,0/16
  12. Attitude Maneuver Control of Spacecraft Using Angular Momentum Exchange,GuoYanNing/Harbin Institute of Technology,0/141
  13. Design of Attitude Control Flyweel System Based on Micro-Planar Motor,ZhangLei/Graduate Schoo,Chinese Academy of Sciences,0/10
  14. Research for Autonomous Navigation of Space Maneuver Vehicle Using SINS/Stellar/Magnetic Measurements,ZhangYuChun/Nanjing University of Aeronautics and Astronautics,0/8
  15. Research on Switching Based Fault Tolerant Control for Satellite Attitude Control Systems,FanZuo/Nanjing University of Aeronautics and Astronautics,0/16
  16. Research of Micro Momentum Wheel Based on Pico-Satellite,WangZhiYuan/Zhejiang University,0/13
  17. A Large-field and High Performance Star Sensor Design,ChenCaiMin/Harbin Institute of Technology,0/78
  18. Research on Spacecraft Attitude Control Based on Fuzzy Sliding Mode Variable Structure Control,ShiZhiHua/East China University of Science and Technology,0/45
  19. Research of Satellite Attitude Control Intelligent Algorithm,LiuHanMin/China University of Geosciences,0/54
  20. Input shaping method in the application of flexible spacecraft attitude maneuver control of,LinBing/Nanjing University of Technology and Engineering,0/15
  21. Research of Sensors with Large Field of View for Micro-Satellite,DingZeWei/Zhejiang University,0/24
  22. Research on control method for a class of control moment gyroscope frame system and experiment,YangHaiZuo/Nanjing University of Technology and Engineering,0/11
  23. Time Optimal Control for Three-axis Stabilized Satellite Reorientation,GuoJinLiang/Harbin Institute of Technology,0/1
  24. Application of the Gyrowheeel Based Attitude Control System for the Small Satellite,ZhangZuo/Harbin Institute of Technology,0/2
  25. Research on the Measurement and Control of the Attitude of the Spacecraft by Gyrowheel,BaoGuoLiang/Harbin Institute of Technology,0/2
  26. Satellite Attitude Control Using Single Gimbal Conrol Moment Gro(SGCMG),YangPeng/Harbin Institute of Technology,0/1
  27. SoC Design for Digital Sun Sensor,FuYongJie/Harbin Institute of Technology,0/4
  28. Study on the Attitude Control System of Satellite with Reaction Wheels and Magnetotors,MaXingYu/Harbin Institute of Technology,0/1
  29. Characteristic Model-based Attitude Control Method and Application Research for Spacecrafts,HanPengWu/Lanzhou Jiaotong University,0/6
  30. Adaptive Robust Control for Spacecraft Attitude System,YuanGuoPing/Harbin Institute of Technology,0/17
  31. Research on Fault Diagnosis and Fault-Tolerant Control of Satellite Attitude Control System,GuanYu/Harbin Institute of Technology,0/13
  32. Model-based Actuator Fault Diagnosis and Its Application to Satellite Attitude Control Systems,GaoChunYan/Harbin Institute of Technology,0/5
  33. Fuzzy Control of Spacecraft Attitude Based on T-S Model,ZhangXiHai/Harbin Institute of Technology,0/2
  34. Research on MTi Inertial Measurement Unit and Testing Platform,QiaoZuoZuo/University of North,0/83
  35. Spacecraft Attitude Determination and Its Semi-physical Simulation Technology Research,ShiQunShan/PLA Information Engineering University,0/106
  36. Research on Aircraft Attitude Determination Algorithms Based on Nonlinear Filtering,LiChao/Hangzhou University of Electronic Science and Technology,0/137
  37. X-ray Pulsar-Based Autonomous Navigation and Its Application to High Earth Orbits Satellites,QiaoLi/Nanjing University of Aeronautics and Astronautics,0/221
  38. Study on Spacecraft Attitude Coordination Control Based on Consensus Algorithm,MengZiYang/Tsinghua University,1/113
  39. Research on the Visual Simulation Technology of Attitude Control for Space Orbit Transfer Vehicle,ZhaoZuo/Shenyang University of Technology,0/44
  40. The Application of Variable Structure Control in Attitude Maneuver of Flexible Spacecraft,LinQian/Harbin Institute of Technology,0/27
  41. Study the Guidance, Autonomous Navigation and Control of Lunar Soft Landing,LiMaoDeng/Harbin Institute of Technology,0/353
  42. Structural Design and Analysis of High Accuracy Star Sensor,WuWei/Xi'an Optics and Fine Mechanics,0/160
  43. Study on the Influence Caused by Temperature to A Thrust Test System for the Attitude Control Engine,MaFei/Dalian University of Technology,0/37
  44. High Resolution Quick Small Satellite Attitude Maneuver Control for Control Moment Gyro,DuLiMin/Graduate Schoo,Chinese Academy of Sciences,0/391
  45. Algorithm research of spacecraft attitude control,MengSiMing/Heilongjiang University,0/70
  46. Taking SGCMG as the satellite attitude actuator guidance and control methods,ZhouChunFeng/Nanjing University of Technology and Engineering,0/81
  47. Optical Navigation Sensor Calibration System Structure Design and Analysis,HanLe/Changchun University of Science and Technology,0/137
  48. Design and Implementation of the Sun Sensor,WangJun/Zhejiang University,0/121
  49. Research on Autonomous SINS/GNSS/CNS Navigation for High Orbit Vehicle Transfering,ChenShaoHua/Nanjing University of Aeronautics and Astronautics,1/184
  50. Research on High-dynamic Small Star Sensor,ZhengXunJiang/Shanghai Jiaotong University,1/287

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