ES2171355A1 - Un sisrema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio. - Google Patents

Un sisrema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio.

Info

Publication number
ES2171355A1
ES2171355A1 ES200002444A ES200002444A ES2171355A1 ES 2171355 A1 ES2171355 A1 ES 2171355A1 ES 200002444 A ES200002444 A ES 200002444A ES 200002444 A ES200002444 A ES 200002444A ES 2171355 A1 ES2171355 A1 ES 2171355A1
Authority
ES
Spain
Prior art keywords
space
trajectories
spacecrafts
modify
trajectory
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
ES200002444A
Other languages
English (en)
Other versions
ES2171355B1 (es
Inventor
Furio Miguel Morales
Fernandez Jose Luis Perez
Gonzalez Manuel Dorado
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.)
CENITA S A
Original Assignee
CENITA S A
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 CENITA S A filed Critical CENITA S A
Priority to ES200002444A priority Critical patent/ES2171355B1/es
Priority to PCT/ES2001/000376 priority patent/WO2002030748A1/es
Priority to AU2001293875A priority patent/AU2001293875A1/en
Publication of ES2171355A1 publication Critical patent/ES2171355A1/es
Application granted granted Critical
Publication of ES2171355B1 publication Critical patent/ES2171355B1/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
    • 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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • 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
    • 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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Un sistema y un método para modificar y controlar trayectorias de ingenios en navegación espacial o aérea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio. De acuerdo con el invento, se consigue modificar de forma controlada la trayectoria de ingenios espaciales, dirigidos, teledirigidos o autónomos, que se desplacen por el espacio; la trayectoria de cuerpos inertes que se desplacen por el espacio; la trayectoria de cohetes, misiles u otros tipos de dispositivos dirigidos o teledirigidos que ejecuten una trayectoria aérea desde que se produce su lanzamiento hasta que alcanzan su objetivo, independientemente de donde se hallen las localizaciones de éstos. La técnica consiste en proporcionar al objeto un momento angular o aprovechar el suyo propio para, mediante la aplicación de un par de fuerzas perpendicular a dicho momento angular, producir un cambio de trayectoria, cuyo radio vendrá determinado por la relación de las intensidades del momento angular y el par de fuerzas.
ES200002444A 2000-10-10 2000-10-10 Un sistema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio. Expired - Fee Related ES2171355B1 (es)

Priority Applications (3)

Application Number Priority Date Filing Date Title
ES200002444A ES2171355B1 (es) 2000-10-10 2000-10-10 Un sistema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio.
PCT/ES2001/000376 WO2002030748A1 (es) 2000-10-10 2001-10-09 Un sistema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio
AU2001293875A AU2001293875A1 (en) 2000-10-10 2001-10-09 System and method for modifying and controlling trajectories of spacecrafts during space or air navigation and to modify trajectories of inert bodies moving in space

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200002444A ES2171355B1 (es) 2000-10-10 2000-10-10 Un sistema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio.

Publications (2)

Publication Number Publication Date
ES2171355A1 true ES2171355A1 (es) 2002-09-01
ES2171355B1 ES2171355B1 (es) 2003-12-01

Family

ID=8495221

Family Applications (1)

Application Number Title Priority Date Filing Date
ES200002444A Expired - Fee Related ES2171355B1 (es) 2000-10-10 2000-10-10 Un sistema y un metodo para modificar y controlar trayectorias de ingenios en navegacion espacial o aerea, y para modificar trayectorias de cuerpos inertes que se desplazan por el espacio.

Country Status (3)

Country Link
AU (1) AU2001293875A1 (es)
ES (1) ES2171355B1 (es)
WO (1) WO2002030748A1 (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101223081A (zh) * 2005-07-12 2008-07-16 应用扭矩及旋转研究中心有限公司（C.I.F.B83987073） 用于加速运动物体的系统
CN106628260B (zh) * 2016-11-17 2018-11-23 上海卫星工程研究所 一种航天器推力器共面双备份的布局设计方法

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
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
US5315158A (en) * 1993-05-17 1994-05-24 Danielson Arnold O Integrated roll control and power supply system and method
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
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
US5315158A (en) * 1993-05-17 1994-05-24 Danielson Arnold O Integrated roll control and power supply system and method
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
AU2001293875A1 (en) 2002-04-22
ES2171355B1 (es) 2003-12-01
WO2002030748A1 (es) 2002-04-18

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