Television antenna directing and tracking system for television program network between air-borne and ground offices

• US 4,047,175 A
• Filed: 03/03/1976
• Issued: 09/06/1977
• Est. Priority Date: 03/05/1975
• Status: Expired due to Term

• Current Assignee: Tokyo Keiso Company
• Original Assignee: Tokyo Keiso Company
• Inventors: Shimizu, Kuniaki, Taira, Hideya
• Primary Examiner(s): Wilbur, Maynard R.
• Assistant Examiner(s): Berger, Richard E.
• Application Number:
  US05/663,529
• Time in Patent Office: 552 Days
• Field of Search: 343/100 CS, 343/117 R, 325/4, 325/14
• US Class Current: 342/359
• CPC Class Codes: G01S 3/42 the desired condition being maintained automatically

Abstract

This invention relates to a television antenna directing and tracking system for directing a television repeating or relaying antenna mounted on an aircraft toward a ground station. The air-borne office is provided with a coordinate transforming device for transforming the azimuth angle φ_A (t) and the elevation angle θ_A (t) which represent the direction of the aircraft with respect to the longitude and latitude of the globe or the globe coordinate into the azimuth angle φ_B (t) and the elevation angle θ_B (t) at the air-borne coordinate. The ground office is equipped with receiving means and tracking means and the air-borne office receives command signals regarding the azimuth angle φ_A (t) and the elevation angle θ_A (t) from the ground office. Further, the air-borne office is equipped with means for computing by itself the azimuth angle φ_A (t) and the elevation angle θ_A (t) based on the flight informations without the aid of the ground office.

Claims

1. An automatic television antenna directing and tracking system comprisinga repeating antenna mounted on an aircraft for repeating television video signals to a ground office;

2. an air-borne station mounted on a said aircraft and including a control system for automatically directing said antenna toward said ground office, said control system including direction angle setting means, coordinate transforming means and an antenna driving unit, said direction angle setting means comprising means for giving the azimuth angle and the elevation angle on the longitude-latitude coordinate as measured from said ground office to said coordinate transforming means for directing said repeating antenna toward said ground office, said coordinate transforming means including means for transforming the azimuth angle and the elevation angle on the longitude-latitude coordinate into the azimuth angle and the elevation angle on the air-borne coordinate based on the azimuth angle of the craft head, pitching angle and the rolling angle of said aircraft, and said antenna driving unit including a servo-loop containing a servo-motor and a gear train for rotating the azimuth angle shaft and the elevation angle shaft of said repeating antenna, and

3. a ground station in said ground office including a repeating receiving installation having a receiving parabola antenna, a tracking installation having a tracking parabola antenna and an angle command communication means, said tracking installation including means for directing said receiving parabola antenna of the repeating receiving installation toward said air-borne station, and said angle command communication means including means for detecting the azimuth angle and the elevation angle of said tracking parabola antenna of said tracking installation and means for transmitting an angle command signal to said air-craft.

2. The automatic television antenna directing and tracking system according to claim 1 wherein said air-borne station comprises means for transforming a unit vector represented by an azimuth angle φ

_A (t) and an elevation angle θ

_A (t) given by said direction angle setting means on the longitude-latitude coordinate utilizing said repeating antenna as the origin into three axes rectangular coordinate components (x_E, Y_E, -z_E), means for transforming said rectangular coordinate components into three axes rectangular coordinate components (x_B, y_B, -z_B) on an air-borne coordinate and means for transforming said rectangular coordinate components (x_B, y_B, -z_B) into the azimuth angle φ

_B (t) and the elevation angle θ

_B (t) of said repeating antenna.

3. The automatic television antenna directing and tracking system according to claim 1 wherein said air-borne station further comprises means for switching the transformation of said three axes rectangular components (x_B, y_B, -z_B) of the unit vector on the air-borne coordinate between the azimuth angle φ

_B (t) and the elevation angle θ

_B (t) of the repeating antenna, and the rolling angle φ

_B (t) and the elevation angle ρ

_B (t) of said repeating antenna, thereby eliminating the dead point locking thereof.

4. The automatic television antenna directing and tracking system according to claim 1 wherein said air-borne station further comprises automatic gain control means for imparting a loop gain proportional to 1/cos θ

_B (t) to a servo-loop including a servo-motor for the azimuth axes of said repeating antenna, where θ

_B (t) represents the elevation angle of said repeating antenna.

5. An automatic television antenna directing and trackin system comprising

12. The automatic television antenna directing and tracking system according to claim 5 wherein said direction angle self setting means comprises error correction means which successively changes said initial point having a coordinate (x_O, y_O) to one of a plurality of initial points predetermined along the flight course of said air-craft.

6. a repeating antenna mounted on an aircraft for repeating television video singals to a ground office,an air-borne station including an antenna driving unit for automatically directing said repeating antenna toward said ground station, direction angle self setting means and coordinate transforming means, said direction angle self setting means including means responsive to a flight information for applying to said coordinate transforming means an azimuth angle and an elevation angle required to direct said repeating antenna toward said ground office, said coordinate transforming means transforming the azimuth angle and the elevation angle on the longitude-latitude coordinate into the azimuth angle and the elevation angle on the air-borne coordinate based on the azimuth angle of the craft head, the pitching angle and the rolling angle of said aircraft, and said antenna driving unit including servo-loops respectively containg a servo-motor and a gear train for rotating the azimuth shaft and the elevation shaft of said repeating antenna, anda ground station in said ground office, said ground station including a receiving installation provided with a receiving parabola antenna, and a tracking installation provided with a tracking parabola antenna and means for directing said receiving parabola antenna of said receiving installation toward said aircraft.

7. The television antenna automatic direction and tracking system according to claim 8 wherein said direction angle self setting means comprises means responsive to a flight information of said aircraft for obtaining the positin coordinate (x_t, y_t, -z_t) of said aircraft, and means for operating the azimuth angle φ

_A (t) and the elevation angle θ

_A (t) of said aircraft in accordance with equations ##EQU17##

8. The automatic television antenna directing and tracking system according to claim 6 wherein said direction angle self setting means further comprises an inertial navigation system for obtaining the values of x_t and y_t, and an altitude meter for producing the value of -z_t.

9. The automatic television antenna directing and tracking system according to claim 6 wherein said direction angle self setting means comprises an operation means for determining said position coordinate in according with equations ##EQU18## where V(t) represents the velocity of the aircraft with respect to the earth, φ

_E (t) the angle of the flight course with respect to the earth, and (x_O, y_O) the position coordinate of an initial point on a predetermined position of the flight course.

10. The automatic television antenna directing and tracking system according to claim 6 wherein said direction self angle setting means comprises computing means for determining the position coordinate (x_t, y_t) of said air-craft for correcting the effect of wind in accordance with the equations ##EQU19## where x_O and y_O represent the coordinate of a predetermined initial point on a prescribed flight course, V_A (t) the true velocity of the aircraft, φ

_A the azimuth angle of the head of the aircraft, φ

_W the direction of the wind provided by navigation weather information and V_W the velocity of wind provided by navigation weather information.

11. The automatic television antenna directing and tracking system according to claim 8 wherein said direction angle self setting means comprises error correction means which successively changes said initial point having a coordinate (x_O, y_O) to one of a plurality of initial points predetermined along the flight course of said aircraft.