FIELD: measuring equipment, applicable for determination of the Sun angular coordinates in the spacecraft coordinate system.
SUBSTANCE: the Sun attitude pickup has an optical system made in the form of a wide-angle lens including an inlet and outlet plano-convex lenses with a diaphragm placed between them, an optical element is positioned in its holes, matrix photodetector, and a unit for processing of information and computation of coordinates. The refractive indices of the optical components are selected proceeding from the relation: n1≥n2<n3, where n1 - the refractive index of the inlet plano-convex lens; n2 - the refractive index of the optical element; n3 - the refractive index of the outlet plano-convex lens.
EFFECT: obtained information in a wide angular field with a high precision.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
OPTICAL SOLAR SENSOR | 2013 |
|
RU2517979C1 |
HORIZON SCANNER | 1991 |
|
RU2014564C1 |
METHOD OF SUN ANGULAR COORDINATES MEASUREMENT AND DEVICE TO THIS END | 2013 |
|
RU2555216C2 |
HEAT LOCATOR | 2016 |
|
RU2604959C1 |
ANGULAR-MOTION TRANSDUCER | 2017 |
|
RU2644994C1 |
THERMAL DIRECTION FINDER | 2008 |
|
RU2396574C2 |
HORIZON SCANNER | 1991 |
|
RU2020419C1 |
ANGLE MEASUREMENT DEVICE | 2011 |
|
RU2470258C1 |
HELMET-MOUNTED TARGET DESIGNATION AND INDICATION SYSTEM AND SIGHT LINE ANGULAR POSITION DETERMINING METHOD ON ITS BASIS | 2017 |
|
RU2674533C1 |
COLLINEAR BEAM TRANSFER DEVICE | 2024 |
|
RU2824311C1 |
Authors
Dates
2007-10-10—Published
2006-10-20—Filed