GB848692A - Improvements in or relating to stellar orientation detector - Google Patents

Improvements in or relating to stellar orientation detector

Info

Publication number
GB848692A
GB848692A GB2753456A GB2753456A GB848692A GB 848692 A GB848692 A GB 848692A GB 2753456 A GB2753456 A GB 2753456A GB 2753456 A GB2753456 A GB 2753456A GB 848692 A GB848692 A GB 848692A
Authority
GB
United Kingdom
Prior art keywords
phase
star
light
axis
reticles
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
GB2753456A
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.)
North American Aviation Corp
Original Assignee
North American Aviation Corp
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 North American Aviation Corp filed Critical North American Aviation Corp
Priority to GB2753456A priority Critical patent/GB848692A/en
Publication of GB848692A publication Critical patent/GB848692A/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
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782Systems for determining direction or deviation from predetermined direction
    • G01S3/787Systems for determining direction or deviation from predetermined direction using rotating reticles producing a direction-dependent modulation characteristic

Abstract

848,692. Photo-electric determination of direction. NORTH AMERICAN AVIATION Inc. Sept. 7, 1956, No. 27534/56. Class 40(3). In order to generate voltages indicative of the deviation of the axis of an optical system from a line of sight to a star, light from the star is split into two beams each directed on to a respective photo-electric cell and means are provided to modulate each beam with a phase relation dependent on both the magnitude and sense of said deviation. The optical system comprises an objective lens 1, Fig. 1, and beam-splitting prisms 2, 3, the light from which falls on photocells 10, 11 respectively after being modulated by rotating reticles 4, 5 respectively. The reticles 4, 5 Fig. 2 are formed with two and three apertures, respectively, bounded by Archimedes spirals having curvatures in the ratio 2:3 and are driven by gears 7, 6, respectively, from gear 9 and motor 8 at speeds in the ratio 3:2. The generator 12, driven by the motor 8, produces a signal S 3 of standard phase at the same frequency as that of the signals S 2 , S 1 respectively arising in the photocells 10, 11, due to the modulation of the light beams by reticles 4, 5. Signals S 1 ,S 2 are fed to a differential synchro 19, Fig. 3, the shaft output of which corresponds to the phase difference # between the signals and hence to the star image angle measured clockwise from the positive Y-axis Fig. 2. This shaft output is doubled by gearbox 20 and causes the phase-shifter 14 to shift the phase of signal S 3 , applied thereto, by an angle 2#. The output S 4 from phase-shifter 14 is fed, together with signal S 2 ,to a differential synchro 16 the shaft output of which is thus proportional to #, the phase angle due to the spiral curvature of the reticle apertures. A mechanical computer 15 receives the quantities # and # as shaft rotations and produces therefrom the rectangular coordinates, y = K# cos # and x = K# sin # ,of the star image in the telescope field, which may be 'used to change the telescope orientation so that its optical axis coincides with the line of sight to the star. Details of a suitable mechanical computer are described, Figs. 5, 6, 7 (not shown). In a modified form of reticle, the spiral portion of the apertures occupies only the central portion, the remainder of the aperture being sector-shaped Fig. 4 (not shown). The modulation effect of a uniform sky background light or a linearly varying background light is avoided by the fact that the centroid of the apertured area of a reticle coincides with the axis of rotation. Specification 848,691 is referred to.
GB2753456A 1956-09-07 1956-09-07 Improvements in or relating to stellar orientation detector Expired GB848692A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2753456A GB848692A (en) 1956-09-07 1956-09-07 Improvements in or relating to stellar orientation detector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2753456A GB848692A (en) 1956-09-07 1956-09-07 Improvements in or relating to stellar orientation detector

Publications (1)

Publication Number Publication Date
GB848692A true GB848692A (en) 1960-09-21

Family

ID=10261149

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2753456A Expired GB848692A (en) 1956-09-07 1956-09-07 Improvements in or relating to stellar orientation detector

Country Status (1)

Country Link
GB (1) GB848692A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156622A (en) * 1984-03-22 1985-10-09 Eltro Gmbh Target location method and apparatus
GB2185870A (en) * 1986-01-28 1987-07-29 Diehl Gmbh & Co Missile guidance

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156622A (en) * 1984-03-22 1985-10-09 Eltro Gmbh Target location method and apparatus
GB2185870A (en) * 1986-01-28 1987-07-29 Diehl Gmbh & Co Missile guidance
GB2185870B (en) * 1986-01-28 1990-03-28 Diehl Gmbh & Co A target-tracking mechanism

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