FIELD: physics.
SUBSTANCE: coordinator of the homing head contains a spherical fairing, a cardan suspension, aiming and stabilisation engines, angle sensors, angular velocity sensors. The first flat mirror is mounted on the inner suspension frame. The intersection point of the rotation axis of the inner frame and the rotation axis of the external suspension frame coincides with the curvature center of the spherical fairing surfaces. On the fixed part of the coordinator, there is the second flat mirror connected with the photosensitive elements.
EFFECT: increasing the viewing angle in the front hemisphere of the homing head, increasing the accuracy of determining the coordinates of the object, reducing the load on the suspension drives and the possibility of obtaining higher dynamic characteristics of the stabilisation system of the optical axis.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
OPTICAL-ELECTRONIC TRACKING COORDINATOR (VERSIONS) | 2008 |
|
RU2395108C2 |
SELF-GUIDANCE ACTIVE LASER HEAD | 2013 |
|
RU2573709C2 |
OPTIC-ELECTRONIC TRACKING COORDINATOR | 2011 |
|
RU2476826C1 |
COMBINED MULTI-CHANNEL HOMING HEAD | 2017 |
|
RU2693028C2 |
AIRCRAFT LANDING SYSTEM | 1994 |
|
RU2086471C1 |
OPTO-ELECTRONIC FOLLOWING DEVICE | 2022 |
|
RU2799891C1 |
METHOD OF CONTROLLING AND STABILISING MOBILE CARRIER, INTEGRATED SYSTEM, DEVICE FOR TURNING ANTENNA REFLECTOR IN TWO MUTUALLY-PERPENDICULAR PLANES AND DEVICE FOR ACTUATING DIFFERENTIAL AERODYNAMIC CONTROLLERS FOR REALISING SAID METHOD | 2009 |
|
RU2423658C2 |
OPTOELECTRONIC TRACKING COORDINATOR | 1996 |
|
RU2101724C1 |
ANTENNA DEVICE WITH LINEAR POLARIZATION | 2005 |
|
RU2282287C1 |
OPTOELECTRONIC POSITION INDICATOR | 1996 |
|
RU2160453C2 |
Authors
Dates
2018-02-15—Published
2016-08-24—Filed