This page left intentionally blank - Seoul National University · 2019. 11. 14. · Attitude disturbance problem is considered as another practical issue. The effect of magnetic torquer

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  • 저작자표시-비영리-변경금지 2.0 대한민국

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  • -

    2018 8

  • Doctoral Committee:

    Professor Chang Don Kee, Chair

    Professor Jai-Ick Yoh

    Professor Chan Gook Park

    Professor In-Seuck Jeung

    Senior Assistant Professor Takaya Inamori

  • -

    2018 6

    2018 8

    : ___________________

    : ___________________

    : ___________________

    : ___________________

    : ___________________

  • I

  • II

  • III

    Table of Contents

    Abstract ............................................................................................................. I

    List of Tables ......................................................................................................... VII

    List of Figures ........................................................................................................ IX

    Chapter 1 Introduction ......................................................................................... 1

    1.1. Background ................................................................................................. 2

    1.2. Motivation................................................................................................... 7

    1.2.1. SNUSAT-1/1b ..................................................................................... 7

    1.2.2. SNUSAT-2 .......................................................................................... 9

    1.3. Literature Review ....................................................................................... 9

    1.3.1. Differential drag .................................................................................. 9

    1.3.2. High specific impulse thruster ........................................................... 13

    1.3.3. High-thrust thruster ........................................................................... 15

    1.3.4. Requirements for novel CubeSat orbit maneuver .............................. 17

    1.4. Contribution .............................................................................................. 19

    1.5. Dissertation outline ................................................................................... 21

    Chapter 2 Interaction between Magnetic Actuator and Space Environment .. 22

    2.1. Magnetic Plasma Drag .............................................................................. 22

    2.1.1. Literature Review .............................................................................. 22

    2.1.2. Space Plasma Environment ............................................................... 23

    2.1.3. Magnetic Field Surrounding a Satellite ............................................. 28

    2.1.4. Charged Particle Motion in Electric and Magnetic Fields................. 30

  • IV

    2.1.5. Particle-In-Cell Simulation ................................................................ 32

    2.2. Geomagnetic Torque ................................................................................ 38

    Chapter 3 Methodology ..................................................................................... 41

    3.1. Plasma Drag Constellation Concept ......................................................... 41

    3.2. Analytical Method .................................................................................... 44

    3.3. Numerical Method .................................................................................... 49

    3.3.1. Constellation Deployment Simulator ................................................ 50

    3.3.2. Attitude Simulator ............................................................................. 60

    Chapter 4 Plasma Drag Constellation ................................................................ 65

    4.1. General Aspects of Plasma Drag Constellation Time ............................... 65

    4.2. Parametric Study of Plasma Drag Constellation ....................................... 65

    Chapter 5 Plasma Drag Constellation Feasibility Analysis ............................... 72

    5.1. Magnetic Moment of a Magnetic Actuator on a CubeSat ........................ 72

    5.2. Perturbation of Right Ascension of the Ascending Node ......................... 74

    5.3. Example of a four-CubeSat plasma drag constellation ............................. 78

    Chapter 6 Geomagnetic Torque Mitigation ....................................................... 81

    6.1. Transition Characteristics of Magnetic Plasma Drag due to Polarity

    Switching............................................................................................................. 81

    6.2. Effect of High-Frequency Polarity Switching .......................................... 83

    6.3. Practical Consideration on High-Frequency Switching ............................ 93

    Chapter 7 Conclusions ....................................................................................... 95

    4.1. Summary ...................................................................................................... 95

    4.2. Future work ................................................................................................ 100

  • V

    4.2.1. In-depth study of disturbance torque cancellation............................... 100

    4.2.2. Advanced simple-IRI model development .......................................... 101

    4.2.3. Large MTQ interface development ..................................................... 101

    Appendix Analytical solution of magnetic plasma drag ....................................... 102

    Bibliography ......................................................................................................... 105

    ......................................................................................................... 114

  • VI

  • VII

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  • VIII

  • IX

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  • X

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  • XI

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  • XII

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  • XIII

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  • XIV

    ..................................................................................................

    ...........................................................

  • 1

    Chapter 1

  • 2

    1.1.

  • 3

    XI-V (1U)

    cm

    1 kg

    SNUSAT-2 (3U)

    cm

    2.85 kg

    SNUSAT-1/1b (2U)

    cm

    1.9 kg

  • 4

    CubeSatsLaunched Each Year CubeSatsby Mission Type

    798 Total

  • 5

  • 6

  • 7

    1.2.

    1.2.1.

  • 8

  • 9

    1.2.2.

    1.3.

    1.3.1.

  • 10

  • 11

  • 12

  • 13

    1.3.2.

  • 14

  • 15

    1.3.3.

    Electronics (0.2 U) Thruster headNeutralizer

  • 16

  • 17

    1.3.4.

  • 18

  • 19

    1.4.

  • 20

  • 21

    1.5.

  • 22

    Chapter 2

    2.1.

    2.1.1.

  • 23

    2.1.2.

  • 24

  • 25

  • 26

  • 27

  • 28

    2.1.3.

  • 29

    x

    y

    Relative

    plasma flow

  • 30

    2.1.4.

  • 31

  • 32

    2.1.5.