GB2015292B - Method for determining the attitude of a spinning spacecraft - Google Patents

Method for determining the attitude of a spinning spacecraft

Info

Publication number
GB2015292B
GB2015292B GB7906941A GB7906941A GB2015292B GB 2015292 B GB2015292 B GB 2015292B GB 7906941 A GB7906941 A GB 7906941A GB 7906941 A GB7906941 A GB 7906941A GB 2015292 B GB2015292 B GB 2015292B
Authority
GB
United Kingdom
Prior art keywords
attitude
determining
spinning spacecraft
spacecraft
spinning
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.)
Expired
Application number
GB7906941A
Other versions
GB2015292A (en
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB7906941A priority Critical patent/GB2015292B/en
Publication of GB2015292A publication Critical patent/GB2015292A/en
Application granted granted Critical
Publication of GB2015292B publication Critical patent/GB2015292B/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S1/00Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
    • G01S1/08Systems for determining direction or position line
    • G01S1/38Systems for determining direction or position line using comparison of [1] the phase of the envelope of the change of frequency, due to Doppler effect, of the signal transmitted by an antenna moving, or appearing to move, in a cyclic path with [2] the phase of a reference signal, the frequency of this reference signal being synchronised with that of the cyclic movement, or apparent cyclic movement, of the antenna
    • G01S1/40Systems for determining direction or position line using comparison of [1] the phase of the envelope of the change of frequency, due to Doppler effect, of the signal transmitted by an antenna moving, or appearing to move, in a cyclic path with [2] the phase of a reference signal, the frequency of this reference signal being synchronised with that of the cyclic movement, or apparent cyclic movement, of the antenna the apparent movement of the antenna being produced by cyclic sequential energisation of fixed antennas
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
    • G01S5/0247Determining attitude
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
    • G01S5/08Position of single direction-finder fixed by determining direction of a plurality of spaced sources of known location

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Navigation (AREA)
GB7906941A 1977-11-30 1979-02-27 Method for determining the attitude of a spinning spacecraft Expired GB2015292B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7906941A GB2015292B (en) 1977-11-30 1979-02-27 Method for determining the attitude of a spinning spacecraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB4973877 1977-11-30
GB7906941A GB2015292B (en) 1977-11-30 1979-02-27 Method for determining the attitude of a spinning spacecraft

Publications (2)

Publication Number Publication Date
GB2015292A GB2015292A (en) 1979-09-05
GB2015292B true GB2015292B (en) 1982-06-23

Family

ID=26266534

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7906941A Expired GB2015292B (en) 1977-11-30 1979-02-27 Method for determining the attitude of a spinning spacecraft

Country Status (1)

Country Link
GB (1) GB2015292B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4883244A (en) * 1987-12-23 1989-11-28 Hughes Aircraft Company Satellite attitude determination and control system with agile beam sensing

Also Published As

Publication number Publication date
GB2015292A (en) 1979-09-05

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee