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GB1229883A - - Google Patents

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Publication number
GB1229883A
GB1229883A GB1229883DA GB1229883A GB 1229883 A GB1229883 A GB 1229883A GB 1229883D A GB1229883D A GB 1229883DA GB 1229883 A GB1229883 A GB 1229883A
Authority
GB
United Kingdom
Prior art keywords
vehicle
signals
control system
space
actuators
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
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 filed Critical
Publication of GB1229883A publication Critical patent/GB1229883A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G7/00Simulating cosmonautic conditions, e.g. for conditioning crews

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

1,229,883. Ground testing space vehicles. FIAT S.p.A. 17 May, 1968 [18 May, 1967], No. 23625/68. Heading B7W. [Also in Division G1] In apparatus for ground testing the attitude control system 7 of a space vehicle 1, a programme unit 9 supplies input signals to the control system 7 whereby actuators 8 apply a torque to the vehicle 1 that deforms a bar 4, which deformation is converted by a pick-up device 5 into an electric signal from which a data processing unit 6 calculates the angular displacement that would be undergone by the vehicle in free flight, signals representing this information then being compared with the input signal from the unit 9. In the embodiment shown, the space vehicle is movable in a fluid bearing 2 about a single axis. In a modification (Fig. 2, not shown) three degrees of freedom are provided in that a partially spherical member attached to the vehicle moves on a fluid cushion in a partially spherical cavity. In the embodiment of Fig. 3 (not shown), a device simulates a celestial reference and a sensing device sends to the control system 7 signals representing the variations in the vehicle attitude with respect to the simulated celestial reference. For simulation of relative motion between the space vehicle and the reference, a computer processes signals from the actuators 8 and transmits signals that move the reference device mechanically.
GB1229883D 1967-05-18 1968-05-17 Expired GB1229883A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT803952 1967-05-18

Publications (1)

Publication Number Publication Date
GB1229883A true GB1229883A (en) 1971-04-28

Family

ID=11125673

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1229883D Expired GB1229883A (en) 1967-05-18 1968-05-17

Country Status (1)

Country Link
GB (1) GB1229883A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT201700116334A1 (en) * 2017-10-16 2019-04-16 Argotec S R L EQUIPMENT AND TEST PROCEDURE FOR SPACE SATELLITES OR SUBSYSTEMS OR SPACE SATELLITE PARTS

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT201700116334A1 (en) * 2017-10-16 2019-04-16 Argotec S R L EQUIPMENT AND TEST PROCEDURE FOR SPACE SATELLITES OR SUBSYSTEMS OR SPACE SATELLITE PARTS

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLE Entries relating assignments, transmissions, licences in the register of patents
PCNP Patent ceased through non-payment of renewal fee