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Обзор работ по астродинамике С1 . Astrodynamics Symposium + A6 Space Debris Symposium (A6.4. Mitigation and Standards) + E2. Student Conference. Общая информация. IAC 2013: 30 симпозиумов, из них: 7 в категории A (Science and Exploration) 6 в категории B (Applications and Operations)

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1.Astrodynamics Symposium+A6 Space Debris Symposium(A6.4. Mitigation and Standards)+E2. Student Conference


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IAC 2013:

  • 30 , :

  • 7 A (Science and Exploration)

  • 6 B (Applications and Operations)

  • 4 C (Technology)

  • 6 D (Infrastructure)

  • 7 E (Space and Society)

  • 3727 (!)

  • 74


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1.1.1

1.4.5 , ,


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C1.1.1Maximum-Likelihood Estimation Optimizer for Constrained, Time-Optimal Satellite ReorientationRobert G. Melton (Penn State, USA)

  • Covariance Matrix Adaptation Evolution Strategy (CMA-ES)

  • -

  • ,


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C1.4.5Precise Spin Sync Slew Control Based on Nonlinear Optimization for Spinning SpacecraftYung-Hua Wu (University of Surrey, UK)

  • ( ),

  • ,

  • , : , ,


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1.2.3 ( )

1.2.6

C1.4.9

1.4.12


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C1.2.3Experimental Demonstration of 3-DOF Capabilities of A Tilted Wheel Using An Air-Bearing TableLawrence Inumoh (Surrey Space Centre, University of Surrey, UK)

  • :


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C1.4.12Attitude Maneuver Control of A Spacecraft by One Variable-Speed Control Moment GyroHaichao Gui (Beihang University, Peoples Republic of China)

  • -

  • :

  • - ,


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1.1.9 (drag balance instrument)

C1.1.11 (- )

1.1.12

1.4.7 PID-


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C1.1.12A Nadir-Pointing Magnetic Attitude Control System for Tigrisat NanosatelliteParide Testani (University of Rome La Sapienza, Italy)

  • Bdot :

  • :

1 2


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1.1.7 -

C1.2.2

1.2.9

1.4.8


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1.1.6

C1.2.1


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C1.1.6Uniform Rotations of A Two-Body Tethered System in An Elliptic OrbitAnna Guerman (University of Beira Interior, Portugal)

  • ,

  • , ,

  • =0, 1, 2, 3, 4

  • ,


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C1.2.1Long Term Dynamics and Control of a Bare Electrodynamic Tethers Under Multi-Environment PerturbationsRui Zhong (York University, Canada)

  • ,

  • 5 1.75 , 0.25 , 500 , 0.5

  • IGRF 77

  • ,

  • 57 3 , 23


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/

1.1.3

1.1.8

1.2.11

1.6.9

1.8.3


C1 1 3 passive aerostability for drag sails gemma saura carretero cranfield university uk

C1.1.3Passive Aerostability for Drag SailsGemma Saura Carretero (Cranfield University, UK)

  • 25- 700


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C1.6.9Optimal Law for Inclination Change in An Atmosphere Through Solar SailingValentin Stolbunov (University of Glasgow, UK)

  • ,


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C1.8.3Agile Solar Sailing in Three-Body Problem:Motion Between Artificial Equilibrium PointsJeannette Heiligers (University of Strathclyde, UK)

  • , ( )

  • ,


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:

1.7.7 - L2 -

C1.7.12 - L1 L2 -

1.8.5 L1 L2 -

1.8.6 -

C1.8.7

1.9.11


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C1.8.5Earth-Sun L1 and L2 to Moon TransfersExploiting Natural DynamicsWillem van der Weg (University of Strathclyde, UK)

  • - ( )

  • () L1/L2 -

    - () L2 -

  • V


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/

1.7.6 Akatsuki: VILT-

C1.7.8 ()

1.9.1


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C1.7.8Earth Resonant Gravity Assistsfor Asteroid Retrieval MissionsJoan Pau Sanchez Cuartielles (University of Strathclyde, UK)

  • L2 - V

  • V


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1.4.3 () -

C1.4.11 ,

1.7.9


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1.3.10 -

C1.5.2 , -

1.5.9

,

1.8.11


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C1.5.9Application of Hamiltonian Structure-Preserving Control to Cluster Flight for Fractionated Spacecraft on An Elliptic OrbitMing Xu (Beihang University, Peoples Republic of China)

  • -

  • ,


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C1.8.11Relative Orbital Dynamics of Swarms of Femto-SpacecraftGiorgio Mingotti (University of Strathclyde, UK)

  • : ,

  • , : , ( ) ( )


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1.4.10

C1.5.3 :

1.5.11

1.5.13 PRISMA: IRIDES

1.6.3


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1.4.1

1.6.11 L5 -

C1.6.13

1.7.10


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C1.6.13A Study on Low-Cost and Flexible Deep-Space Exploration Utilizing A Concept of Interplanetary Parking OrbitToshinori Ikenaga (JAXA, Japan)

  • :

    ,

  • :

    1-2


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1.3.11 N , -

C1.6.2 ( , )

1.6.5 /


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1.6.7 ( + ) :

C1.6.10

1.7.4 Electra:


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C1.6.7Novel Numerical Optimisation of the Hohmann Spiral TransferSteven Owens (University of Strathclyde, UK)

  • ( ),

  • 10%


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1.7.11 1996 FG3

C1.9.3

1.9.4

1.9.5 ,

1.9.6 ,


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1.3.8

C1.3.9 ( )

1.4.6 ( SINPLEX FP7)

1.4.13

1.5.8

1.5.10

1.6.11


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1.3.5

1.4.2 -

1.8.9

1.9.8


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1.2.4 unscented (AUKF)

C1.3.6 H2/H-


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C1.2.4A Residual-Based Adaptive Unscented Kalman Filter for MicrosatellitesLe Xuan Huy (Tokyo Institute of Technology, Japan)

  • Unscented Kalman Filter (UKF)

  • ,

  • UKF: ,

  • UKF AUKF


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C1.3.6A Mixed Kalman/H-Infinity Filtering Approach for Augmented Proportional Navigation GuidanceAdrian-Mihail Stoica (University Politehnica of Bucharest, Romania)

  • (H2-) ,

  • H-, , ( )

  • H2/H-: H2- H


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1.6.1 ,

C1.6.4

1.8.2


A6 4 mitigation and standards

A6.4. Mitigation and Standards

A6.4.4 DRAMA 2.0:

( ESA)

A6.4.6 3U-CubeSat ( Deorbitsail FP7, - Surrey Space Centre, University of Surrey, UK)

A6.4.8 (Tohoku University, Japan)


E2 student conference

E2. Student Conference

Undergraduate Students

Gold Emilien Fabacher Finding Multiple Sun-Earth Saddle-Point Flybys for LISA Pathfinder (France)

Silver Anja Schuster New Options for the Mercury Orbit Insertion of BepiColombo (Germany)

Graduate Students

Gold Florian Reichel Design, Test and Verification of A Miniature Attitude Control System for the Picosatellite UWE-3 (Germany)

Best Technical Paper

Irfan Rashed Attitude Determination of Nano-Satellites Using Low-Cost, Quadrant Based MEMS Sun Sensors for Creating Unique Sensor Fusion (Republic of Korea)


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