ES2180367A1 - Nuevo procedimiento para modificar la trayectoria de un cuerpo movil o particula. - Google Patents

Nuevo procedimiento para modificar la trayectoria de un cuerpo movil o particula.

Info

Publication number
ES2180367A1
ES2180367A1 ES200000491A ES200000491A ES2180367A1 ES 2180367 A1 ES2180367 A1 ES 2180367A1 ES 200000491 A ES200000491 A ES 200000491A ES 200000491 A ES200000491 A ES 200000491A ES 2180367 A1 ES2180367 A1 ES 2180367A1
Authority
ES
Spain
Prior art keywords
angular momentum
application
moving body
movement
modification technique
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
ES200000491A
Other languages
English (en)
Other versions
ES2180367B1 (es
Inventor
Gonzalez Manuel Dorado
Fernandez Jose Luis Perez
Furio Miguel Morales
Urena Angel Gonzalez
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CT DE INVESTIGACION DE TECN AE
Original Assignee
CT DE INVESTIGACION DE TECN AE
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 CT DE INVESTIGACION DE TECN AE filed Critical CT DE INVESTIGACION DE TECN AE
Priority to ES200000491A priority Critical patent/ES2180367B1/es
Publication of ES2180367A1 publication Critical patent/ES2180367A1/es
Application granted granted Critical
Publication of ES2180367B1 publication Critical patent/ES2180367B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • G—PHYSICS
    • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21K—HANDLING OF PARTICLES OR IONISING RADIATION NOT OTHERWISE PROVIDED FOR; IRRADIATION DEVICES; GAMMA RAY OR X-RAY MICROSCOPES
    • G21K1/00—Arrangements for handling particles or ionising radiation, e.g. focusing or moderating
    • G21K1/08—Deviation, concentration or focusing of the beam by electric or magnetic means

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Navigation (AREA)

Abstract

El nuevo procedimiento para modificar la trayectoria de un cuerpo móvil o partícula se fundamenta en el comportamiento especial de un cuerpo o partícula cuando posee momento angular, se desplaza y se le aplica un par de fuerzas. El cuerpo o la partícula puede disponer de momento angular o se le proporcionará en el caso de que no disponga de él o no sea adecuado. Una vez que el cuerpo en movimiento dispone del momento angular adecuado, la modificación de la trayectoria se conseguirá mediante la aplicación de un par de fuerzas no paralelo al momento angular. Este procedimiento puede aplicarse con grandes ventajas en las siguientes áreas de la técnica: navegación, seguridad en vehículos, instrumentación para metrología análisis instrumental, métodos de concentración y purificación.
ES200000491A 2000-03-01 2000-03-01 Nuevo procedimiento para modificar la trayectoria de un cuerpo movil o particula. Expired - Fee Related ES2180367B1 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES200000491A ES2180367B1 (es) 2000-03-01 2000-03-01 Nuevo procedimiento para modificar la trayectoria de un cuerpo movil o particula.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200000491A ES2180367B1 (es) 2000-03-01 2000-03-01 Nuevo procedimiento para modificar la trayectoria de un cuerpo movil o particula.

Publications (2)

Publication Number Publication Date
ES2180367A1 true ES2180367A1 (es) 2003-02-01
ES2180367B1 ES2180367B1 (es) 2004-04-01

Family

ID=8492521

Family Applications (1)

Application Number Title Priority Date Filing Date
ES200000491A Expired - Fee Related ES2180367B1 (es) 2000-03-01 2000-03-01 Nuevo procedimiento para modificar la trayectoria de un cuerpo movil o particula.

Country Status (1)

Country Link
ES (1) ES2180367B1 (es)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3866025A (en) * 1972-03-17 1975-02-11 Rca Corp Spacecraft attitude control system
US4047026A (en) * 1976-01-02 1977-09-06 Bell Telephone Laboratories, Incorporated Deflection of atomic beams with isotope separation by optical resonance radiation using stimulated emission and the A.C. Stark effect
US4288051A (en) * 1976-09-18 1981-09-08 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Method and apparatus for controlling a satellite
US5222023A (en) * 1991-04-02 1993-06-22 Space Systems/Loral, Inc. Compensated transition for spacecraft attitude control
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
EP0937644A2 (en) * 1998-02-23 1999-08-25 Space Systems/Loral, Inc. Space craft axis stabilizer apparatus, system and method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3866025A (en) * 1972-03-17 1975-02-11 Rca Corp Spacecraft attitude control system
US4047026A (en) * 1976-01-02 1977-09-06 Bell Telephone Laboratories, Incorporated Deflection of atomic beams with isotope separation by optical resonance radiation using stimulated emission and the A.C. Stark effect
US4288051A (en) * 1976-09-18 1981-09-08 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Method and apparatus for controlling a satellite
US5222023A (en) * 1991-04-02 1993-06-22 Space Systems/Loral, Inc. Compensated transition for spacecraft attitude control
US5335179A (en) * 1992-12-24 1994-08-02 General Electric Co. Unified spacecraft attitude control system with pseudo-complementary paired thrusters
EP0937644A2 (en) * 1998-02-23 1999-08-25 Space Systems/Loral, Inc. Space craft axis stabilizer apparatus, system and method

Also Published As

Publication number Publication date
ES2180367B1 (es) 2004-04-01

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