3implementing the tracking algorithms, 1 location information, 2 antenna scale factors – Research Concepts RC2000C User Manual

Page 36: 3 antenna radiation pattern, 3 implementing the tracking algorithms

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RC2000C Az/El Tracking Antenna Controller

Chapter 4

Inclined Orbit Satellites

Research Concepts, Inc. • 5420 Martindale Road • Shawnee, Kansas • 66218-9680 • USA

www.researchconcepts.com

Figure 4.2 – Intelli-Search

4.3 Implementing the Tracking Algorithms

This section describes the information needed to implement the tracking algorithms. The purpose of

this section is to give the user insights into the operation of the controller and to prepare for the actual

entry of the setup information in the following sections.

4.3.1 Location Information

The Antenna Latitude, Antenna Longitude, and the Longitude of the inclined orbit satellite to be tracked

must be specified in order to determine the satellite's apparent motion. In most cases the satellite's

apparent motion as seen by the antenna mount is a skewed figure eight shape. This information is

needed to implement the controller's Intelli-Search algorithm.

4.3.2 Antenna Scale Factors

The azimuth and elevation scale factors refer to the mapping of antenna azimuth and elevation position

counts to antenna azimuth and elevation angles. The elevation scale factor is entered by the user. The

azimuth scale factor can either be specified by the user, or it can be derived from the position and

longitude data of adjacent geostationary satellites.

Scale factor information is entered into the controller via the Azim Constant and Elev Constant CONFIG

mode items. A non-zero value for the Elev Constant must be entered into the controller. If the Azim

Constant CONFIG mode item is initialized to a non-zero value, that value is used as the azimuth scale

factor. If the Azim Constant is initialized to a value of zero, the controller calculates the azimuth scale

factor based on the position and longitude data of geostationary satellites in the vicinity of the inclined

orbit satellite.

If the Azim Constant has a value of zero at least two geostationary satellites must be programmed into

memory (via SETUP mode) before a track may be initiated on an inclined orbit satellite. For this case it

is also very important that the proper longitude values be specified for geostationary satellites which are

programmed into the controller's memory. If a geostationary satellite is programmed into memory with

an incorrect longitude value (angle or direction), the controller will accurately position the antenna on

the geostationary satellite when it is recalled via AUTO mode, but may not track an inclined orbit

satellite properly which is located in the vicinity of the geostationary satellite. Verify the longitude

value of all satellites programmed into the controller via setup mode if the controller is using

geostationary satellites to determine the azimuth scale factor.

4.3.3 Antenna Radiation Pattern

The antenna radiation pattern specifies antenna receive power versus antenna pointing angle relative to

boresight. Boresight is the pointing angle associated with maximum received power from a given

satellite. The controller calculates the shape of the antenna's radiation pattern by knowing the Antenna

Size and the frequency Band (L, C or Ku) currently in use. Antenna Size data is entered via a CONFIG

mode prompt. The frequency Band data is specified in SETUP mode when the user initiates a track on

an inclined orbit satellite. Note that the controller also allows the user to specify a dual band inclined

orbit satellite. For this case the user is prompted to supply frequency band data on entry into TRACK

mode, and is allowed to change the Frequency Band via the TRACK mode menu.

Antenna radiation pattern information is necessary to allow the user to specify a maximum allowable

antenna pointing error (Max Track Error) in tenths of decibels (dB) rather than in elevation and azimuth

position counts. The Maximum Track Error is used to determine the step size and the frequency of

antenna movement in the STEP TRACK and PROGRAM TRACK sub-modes. In addition, antenna

radiation pattern information is used in SEARCH mode to determine the width of the parallelogram-

shaped search region, and the angle between successive sweeps.

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