IT202300011844A1 - METHOD AND APPARATUS FOR STABILIZING SATELLITE FORMATIONS - Google Patents

METHOD AND APPARATUS FOR STABILIZING SATELLITE FORMATIONS

Info

Publication number
IT202300011844A1
IT202300011844A1 IT102023000011844A IT202300011844A IT202300011844A1 IT 202300011844 A1 IT202300011844 A1 IT 202300011844A1 IT 102023000011844 A IT102023000011844 A IT 102023000011844A IT 202300011844 A IT202300011844 A IT 202300011844A IT 202300011844 A1 IT202300011844 A1 IT 202300011844A1
Authority
IT
Italy
Prior art keywords
stabilizing
satellite formations
formations
stabilizing satellite
satellite
Prior art date
Application number
IT102023000011844A
Other languages
Italian (it)
Inventor
Marcello Romano
Stefano Aliberti
Riccardo Apa
Catello Leonardo Matonti
Original Assignee
Torino Politecnico
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Torino Politecnico filed Critical Torino Politecnico
Priority to IT102023000011844A priority Critical patent/IT202300011844A1/en
Priority to PCT/IB2024/055394 priority patent/WO2024252252A1/en
Publication of IT202300011844A1 publication Critical patent/IT202300011844A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/648—Tethers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1085—Swarms and constellations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242—Orbits and trajectories
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/411—Electric propulsion

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
IT102023000011844A 2023-06-09 2023-06-09 METHOD AND APPARATUS FOR STABILIZING SATELLITE FORMATIONS IT202300011844A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
IT102023000011844A IT202300011844A1 (en) 2023-06-09 2023-06-09 METHOD AND APPARATUS FOR STABILIZING SATELLITE FORMATIONS
PCT/IB2024/055394 WO2024252252A1 (en) 2023-06-09 2024-06-03 Method and apparatus for the stabilisation of a satellite formation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT102023000011844A IT202300011844A1 (en) 2023-06-09 2023-06-09 METHOD AND APPARATUS FOR STABILIZING SATELLITE FORMATIONS

Publications (1)

Publication Number Publication Date
IT202300011844A1 true IT202300011844A1 (en) 2024-12-09

Family

ID=87889473

Family Applications (1)

Application Number Title Priority Date Filing Date
IT102023000011844A IT202300011844A1 (en) 2023-06-09 2023-06-09 METHOD AND APPARATUS FOR STABILIZING SATELLITE FORMATIONS

Country Status (2)

Country Link
IT (1) IT202300011844A1 (en)
WO (1) WO2024252252A1 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3582016A (en) 1967-10-03 1971-06-01 Bernard C Sherman Satellite attitude control mechanism and method
CN107031872A (en) * 2016-10-25 2017-08-11 杭州电子科技大学 Mechanism is recombinated for the formation flight of space rope system
US20230131644A1 (en) * 2021-10-21 2023-04-27 Viridian Space Corporation Turbomolecular Air-Scoop for Satellite Air-Breathing Electric Propulsion

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3582016A (en) 1967-10-03 1971-06-01 Bernard C Sherman Satellite attitude control mechanism and method
CN107031872A (en) * 2016-10-25 2017-08-11 杭州电子科技大学 Mechanism is recombinated for the formation flight of space rope system
US20230131644A1 (en) * 2021-10-21 2023-04-27 Viridian Space Corporation Turbomolecular Air-Scoop for Satellite Air-Breathing Electric Propulsion

Non-Patent Citations (7)

* Cited by examiner, † Cited by third party
Title
APA, R.QUADRELLI, M. B.BEAUCHAMP, A. M.: "IEEE Aerospace Conference (AERO)", March 2022, IEEE., article "Dynamics and Control of helical Arrays in Low Earth Orbit", pages: 1 - 20
GREENE M ET AL: "Tension sensor for tethered satellites", SYSTEM THEORY, 1989. PROCEEDINGS., TWENTY-FIRST SOUTHEASTERN SYMPOSIUM ON TALLAHASSEE, FL, USA 26-28 MARCH 1989, WASHINGTON, DC, USA,IEEE COMPUT. SOC. PR, US, 26 March 1989 (1989-03-26), pages 300 - 304, XP010015541, ISBN: 978-0-8186-1933-5, DOI: 10.1109/SSST.1989.72481 *
HAO WEN ET AL: "Advances in dynamics and control of tethered satellite systems", ACTA MECHANICA SINICA, SPRINGER, BERLIN, DE, vol. 24, no. 3, 9 May 2008 (2008-05-09), pages 229 - 241, XP019598007, ISSN: 1614-3116 *
KESHMIRI MEHDI ; ET AL: "Effects of Aerodynamic Lift on the Stability of Tethered Satellite Systems", ADVANCES IN ASTRONAUTICAL SCIENCES., vol. 42, no. 3, 1 January 1993 (1993-01-01), US, pages 301 - 318, XP093104513, ISSN: 0065-3438 *
MORI OSAMU ET AL: "Coordinated control of tethered satellite cluster systems", AIAA PAPER, 6 August 2001 (2001-08-06), US, XP093104512, ISSN: 0146-3705 *
NOHMI M ET AL: "Path planning for a tethered space robot", ROBOTICS AND AUTOMATION, 1997. PROCEEDINGS., 1997 IEEE INTERNATIONAL C ONFERENCE ON ALBUQUERQUE, NM, USA 20-25 APRIL 1997, IEEE, NEW YORK, NY, USA, vol. 4, 20 April 1997 (1997-04-20), pages 3062 - 3067, XP010235431, ISBN: 978-0-7803-3612-4, DOI: 10.1109/ROBOT.1997.606753 *
PINES D J ET AL: "TWO NONLINEAR CONTROL APPROACHES FOR RETRIEVAL OF A THRUSTING TETHERED SUBSATELLITE", JOURNAL OF GUIDANCE AND CONTROL AND DYNAMICS, AIAA, RESTON, VA, US, vol. 13, no. 4, 1 July 1990 (1990-07-01), pages 651 - 658, XP000209068, ISSN: 0731-5090 *

Also Published As

Publication number Publication date
WO2024252252A1 (en) 2024-12-12

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