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ISSN 2070-7401 (Print), ISSN 2411-0280 (Online)
Sovremennye problemy distantsionnogo zondirovaniya Zemli iz kosmosa
CURRENT PROBLEMS IN REMOTE SENSING OF THE EARTH FROM SPACE

  

Sovremennye problemy distantsionnogo zondirovaniya Zemli iz kosmosa, 2023, Vol. 20, No. 6, pp. 157-164

Experience in applying the algorithm for unloading the flywheel engine using magnetic actuators to ensure the stabilization of the Aist-2D remote sensing satellite

A.N. Bormotov 1 , D.I. Orlov 2 , E.S. Khnyryova 2 , M.E. Bratkova 2 
1 Penza State Technological University, Penza, Russia
2 Samara National Research University, Samara, Russia
Accepted: 06.09.2023
DOI: 10.21046/2070-7401-2023-20-6-157-164
The paper proposes an algorithm for unloading the executive bodies of the motion control system of a small spacecraft for remote sensing of the Earth. Numerical simulation has been carried out which confirms the effectiveness of the algorithm. When implementing the algorithm, data from the angular velocity measurements of the Aist-2D small remote sensing spacecraft rotation using gyroscopic angular velocity vector meters were used. Measurements of the Earth’s magnetic field induction vector, performed using MAGKOM equipment, were also used. As a result of implementing the proposed algorithm for unloading flywheel engines, the dependence of the flywheel angular velocity was obtained. This algorithm can be used to reduce the kinetic moment of the small spacecraft flywheel engines using electromagnets. The study is based on the theorem on the change of the kinetic moment and the introduction of the unloading admissibility criterion. Flywheel engines are considered as the main executive bodies. Magnetic executive bodies are used to reduce the flywheel engine kinetic moment. The study was carried out on the example of the small Aist-2D spacecraft for remote sensing of the Earth. The results of the work can be used to improve the efficiency of small spacecraft motion control system. It will make it possible to improve the resolution of objects imaging from small spacecrafts for remote sensing of the Earth.
Keywords: small Earth remote sensing spacecraft, flywheel engine, magnetic actuators, unloading algorithm
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References:

  1. Abrashkin V. I., Voronov K. E., Dorofeev A. S. et al., Determining the small spacecraft Aist-2D attitude motion by measurements of the equipment KMU-1, Keldysh Institute Preprints, Moscow, 2017, No. 57, 37 p. (in Russian), DOI: 10.20948/prepr-2017-57.
  2. Zubov N. E., Mikrin E. A., Negodyaev S. S., Ryabchenko V. N., Bogachev A. V., Vorobyova E. A., Synthesis of a three-channel system for unloading the kinetic moment of inertial actuators of a spacecraft for circular orbits, Aerospace Research. Proc. MIPT, 2013, Vol. 5, No. 4, pp. 18–25 (in Russian).
  3. Kirilin A. N., Akhmetov R. N., Shakhmatov E. V. et al., Opytno-tekhnologicheskii malyi kosmicheskii apparat “Aist-2D” (Experimental technological small spacecraft Aist-2D), Samara: Publ. House of the Samara Scientific Center RAS, 2017, 324 p.
  4. Kovalenko A. P., Magnitnye sistemy upravleniya kosmicheskimi letatel’nymi apparatami (Magnetic control systems for space aircraft), Moscow: Mechanical Engineering, 1975, 248 p. (in Russian).
  5. Raushenbach B. V., Tokar E. N., Upravlenie orientatsiei kosmicheskikh apparatov (Spacecraft orientation control), Moscow: Nauka Publ. House, 1974, 600 p. (in Russian).
  6. Simonyants R. P., Galkin D. I., Permanent magnet as an unloading tool of the spacecraft reaction wheels, Science and Education of the Bauman MSTU, 2014, Vol. 12, pp. 463–479 (in Russian), DOI: 10.7463/1214.0752094.
  7. Shipov M. G., Reduction of angular velocities of Aist-2D spacecraft using a system of kinetic moment dumping, Vestnik of Samara University Aerospace and Mechanical Engineering, 2019, Vol. 18, No. 2, pp. 121–127 (in Russian), https://doi.org/10.18287/2541-7533-2019-18-2-121-127.
  8. Abrashkin V. I., Voronov K. E., Dorofeev A. S. et al., Detection of the rotational motion of the Aist-2D small spacecraft by magnetic measurements, Cosmic Research, 2019, Vol. 57, No. 1, pp. 48–60, https://doi.org/10.1134/S0010952519010015.
  9. Anshakov G. P., Belousov A. I., Sedel’nikov A. V., The problem of estimating microaccelerations aboard Foton-M4 spacecraft, Russian Aeronautics, 2017, Vol. 60, No. 1, pp. 83–89, https://doi.org/10.3103/S1068799817010123.
  10. Anshakov G. P., Belousov A. I., Sedel’nikov A. V., Gorozhankina A. S., Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion, Russian Aeronautics, 2018, Vol. 61, No. 3, pp. 347–354, https://doi.org/10.3103/S1068799818030054.
  11. Anshakov G. P., Belousov A. I., Sedel’nikov A. V., Puzin Yu.Ya., Effect of the mission and supporting equipment on operation of the magnetometer sensors of the Foton-M No. 2 spacecraft, Russian Aeronautics, 2019, Vol. 62, No. 4, pp. 571–576, https://doi.org/10.3103/S1068799819040068.
  12. Belousov A. I., Sedelnikov A. V., Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation, Russian Aeronautics, 2014, Vol. 57, No. 2, pp. 111–117, https://doi.org/10.3103/S1068799814020019.
  13. Ceamanos X., Moparthy S., Carrer D., Seidel F. C., Assessing the Potential of Geostationary Satellites for Aerosol Remote Sensing Based on Critical Surface Albedo, Remote Sensing, 2019, Vol. 11, No. 24, Article 2958, https://doi.org/10.3390/rs11242958.
  14. Hall C. D., Spinup dynamics of gyrostats, J. Guidance Control and Dynamics, 1995, Vol. 18, No. 5, pp. 1177–1183, https://doi.org/10.2514/3.21522.
  15. Howe D., Magnetic actuators, Sensors and Actuators A: Physical, 2000, Vol. 81, No. 1–3, pp. 268–274, https://doi.org/10.1016/S0924-4247(99)00174-0.
  16. Ivliev N., Evdokimova V., Podlipnov V. et al., First Earth-Imaging CubeSat with Harmonic Diffractive Lens, Remote Sensing, 2022, Vol. 14, No. 9, Article 2230, https://doi.org/10.3390/rs14092230.
  17. Pasciuto I., Ligorio G., Bergamini E. et al., How Angular Velocity Features and Different Gyroscope Noise Types Interact and Determine Orientation Estimation Accuracy, Sensors, 2015, Vol. 15, No. 9, pp. 23983–24001, https://doi.org/10.3390/s150923983.
  18. Sedelnikov A. V., Fast Analysis of Onboard Measurements of the Earth Magnetic Field for the Purpose of Microaccelerations Decrement on Board of the Aist Small Spacecraft During its Uncontrolled Orbital Flight, Intern. Review of Aerospace Engineering, 2018, Vol. 11, No. 2, pp. 76–83, https://doi.org/10.15866/irease.v11i2.13238.
  19. Sedelnikov A. V., The Assessment Problem of Microaccelerations at the Experimental Sample of the Small Spacecraft Aist after the Battery Degradation and the Method of its Solution, Microgravity Science and Technology, 2020, Vol. 32, No. 4, pp. 673–679, https://doi.org/10.1007/s12217-020-09789-w.
  20. Sedelnikov A. V., Algorithm for restoring information of current from solar panels of a small spacecraft prototype Aist with help of normality conditions, J. Aeronautics, Astronautics, and Aviation, 2022, Vol. 54, No. 1, pp. 67–76. DOI: 10.6125/JoAAA.202203_54(1).05.
  21. Sedelnikov A. V., Orlov D. I., Analysis of the significance of the influence of various components of the disturbance from a temperature shock on the level of microaccelerations in the internal environment of a small spacecraft, Microgravity Science and Technology, 2021, Vol. 33, No. 2, Article 22, https://doi.org/10.1007/s12217-020-09867-z.
  22. Sedelnikov A. V., Potienko K. I., Analysis of reduction of controllability of spacecraft during conducting of active control over microaccelerations, Intern. Review of Aerospace Engineering, 2017, Vol. 10, No. 3, pp. 160–166, https://doi.org/10.15866/irease.v10i3.12342.
  23. Sedelnikov A. V., Salmin V. V., Modeling the disturbing effect on the Aist small spacecraft based on the measurements data, Scientific Reports, 2022, Vol. 12, Article 1300, https://doi.org/10.1038/s41598-022-05367-9.
  24. Sedelnikov A. V., Filippov A. S., Gorozhakina A. S. (2018a), Evaluation of calibration accuracy of magnetometer sensors of Aist small spacecraft, J. Physics: Conf. Ser., 2018, Vol. 1015, Article 032045, https://doi.org/10.1088/1742-6596/1015/3/032045.
  25. Sedelnikov A. V., Filippov A. S., Ivashova T. A. (2018b), Earth’s magnetic field measurements data accuracy evaluation on board of the small spacecraft Aist flight model, Jordan J. Mechanical and Industrial Engineering, 2018, Vol. 12, No. 4, pp. 253–260.
  26. Sedelnikov A. V., Khnyryova E. S., Filippov A. S., Ivashova T. A., Measurements Analysis of the Earth’s Magnetic Field Data Obtained from the Flight Model of Aist Small Spacecraft, Intern. J. Mechanical Engineering and Robotic Research, 2019, Vol. 8, No. 4, pp. 542–546, https://doi.org/10.18178/ijmerr.8.4.542-546.
  27. Wang M., Fan C., Yang B. et al., On-Ground Processing of Yaogan-24 Remote Sensing Satellite Attitude Data and Verification Using Geometric Field Calibration, Sensors, 2016, Vol. 16, No. 8, Article 1203, https://doi.org/10.3390/s16081203.