Antenna adjusting apparatus and antenna adjusting method
An antenna adjusting apparatus comprises a sensor that acquires attitude information; a movable axis acquiring unit that acquires a plurality of vectors corresponding to the plurality of axes respectively by acquiring a change in output of the sensor for each of the axes; a first direction acquiring unit that acquires a first direction corresponding to a directional axis of the antenna; a second direction acquiring unit that acquires a second direction, which is a direction with which the directional axis of the antenna is to be aligned; and a calculating unit that calculates, for each of the axes, a correction angle, using the plurality of vectors, wherein the first direction and the second direction are expressed by an Earth-based coordinate system.
1. An antenna adjusting apparatus used for adjusting an attitude of an antenna having directionality and being capable of changing an attitude thereof to be changed by a plurality of axes, the antenna adjusting apparatus comprising:
a sensor configured to acquire information relating to an attitude in a three-dimensional space, the sensor configured to acquire a direction of gravitational force, a true north direction, and GPS coordinates;
a movable axis acquiring unit configured to acquire a plurality of vectors corresponding to the plurality of axes respectively by acquiring a change in output of the sensor for each of the axes when the antenna mounted with the sensor is rotated around each of the axes;
a first direction acquiring unit configured to acquire a first direction corresponding to a directional axis of the antenna, based on the direction of gravitational force, the true north direction, and the GPS coordinates;
a second direction acquiring unit configured to acquire a second direction, which is a direction with which the directional axis of the antenna is to be aligned; and
a calculating unit configured to calculate, for each of the axes, a correction angle, which is an angle by which the antenna is to be rotated in order to make the first direction and the second direction coincide with each other, using the plurality of vectors, wherein
the first direction and the second direction are expressed by an Earth-based coordinate system.
2. The antenna adjusting apparatus according to claim 1 , wherein
the second direction acquiring unit is configured to determine the second direction using the GPS coordinates acquired by the sensor and positional information of a satellite stored in advance.
3. The antenna adjusting apparatus according to claim 1 , wherein
the first direction acquiring unit is configured to acquire sensor position information, which is information relating to a mounting position of the sensor on the antenna, and to acquire the first direction further using the information.
4. The antenna adjusting apparatus according to claim 3 , wherein
the antenna includes one or more sensor bases for mounting the sensor, and
the first direction acquiring unit is configured to acquire sensor position information corresponding to the sensor base, to which the sensor is mounted.
5. The antenna adjusting apparatus according to claim 1 , wherein
the first direction and the second direction are expressed using the ECEF coordinate system.
6. The antenna adjusting apparatus according to claim 1 , further comprising
a driving unit configured to change the attitude of the antenna by rotating the antenna around the plurality of axes, wherein
the calculating unit is configured to calculate a correction angle necessary for tracking a satellite at a prescribed period, and the driving unit is configured to correct the attitude of the antenna, based on the calculated correction angle.
7. The antenna adjusting apparatus according to claim 1 , wherein
the plurality of axes are constituted by an axis corresponding to an azimuth and an axis corresponding to an elevation.
8. An antenna adjusting method of adjusting an attitude of an antenna having directionality and being capable of changing an attitude thereof by a plurality of axes,
the antenna adjusting method comprising:
a movable axis acquiring step of acquiring a plurality of vectors corresponding to each of the plurality of axes by acquiring a change in output of a sensor for each of the axes when the antenna mounted with the sensor is rotated around each of the axes, the sensor being configured to acquire information relating to an attitude in a three-dimensional space, said information including a direction of gravitational force, a true north direction, and GPS coordinates;
a first direction acquiring step of acquiring a first direction corresponding to a directional axis of the antenna, based on the direction of gravitational force, the true north direction, and the GPS coordinates;
a second direction acquiring step of acquiring a second direction, which is a direction with which the directional axis of the antenna is to be aligned; and
a calculation step of calculating, for each of the axes, a correction angle, which is an angle by which the antenna is to be rotated in order to make the first direction and the second direction coincide with each other, using the plurality of vectors, wherein
the first direction and the second direction are expressed by an Earth-based coordinate system.