Automated telescope alignment and orientation method
View Patent ↗A fully automated telescope system is able to be fully operable in both Alt-Az and polar configurations. In either configuration, the telescope aligns itself to the celestial coordinate system following a simplified initialization procedure during which the telescope tube is first pointed north and then pointed towards a user's horizon. A command processor, under application software program control orients the telescope system with respect to the celestial coordinate system given the initial directional inputs. The initial telescope orientation may be further refined by initially inputting a geographical location indicia, or by shooting one or two additional celestial objects. Once the telescope's orientation with respect to the celestial coordinate system is established, the telescope system will automatically move to and track any desired celestial object without further alignment invention by a user.
1. In a computerized telescope system of the type including a telescope coupled for rotation about two orthogonal axes, together with first and second axial position indicators, one coupled to each axis, a method for orienting the telescope system with respect to a spherical coordinate system, the method comprising:
activating a central control processor, the central processor connected to receive positional information from each position indicator;
using the central control processor to receive a rotation metric, the rotation metric rotating a virtual telescope position in the spherical coordinate system in accord with a major axis of the spherical coordinate system;
using the central control processor to receive a geographic input;
moving the telescope about a first one of the axes to a first terrestrial reference position;
communicating, between the central control processor and the first axial position indicator, a first reference value corresponding to the first terrestrial reference position;
moving the telescope about the second one of the axes to a second terrestrial reference position;
communicating, between the central control processor and the second axial position indicator, a second reference value corresponding to the second terrestrial reference position; and
processing the first and second reference values and the rotation metric so as to define a virtual coordinate location of the telescope system with respect to the spherical coordinate system.
2. The method according to claim 1 , further comprising:
accessing a database of celestial objects;
automatically selecting a celestial object, known to be above an observer's horizon, from the database; and
automatically moving the telescope to point towards the selected celestial object.
3. The method according to claim 2 ,
reading a first set of positional data from the respective axial position indicators when the telescope is pointing towards the selected celestial object;
evaluating the position of the selected celestial object in a viewing field of the telescope;
positioning the selected celestial object in a central region of the viewing field;
reading a second set of positional data from the respective axial position indicators when the selected celestial object is positioned in the central region of the viewing field; and
processing the first and second sets of positional reference data to refine the virtual coordinate location of the telescope system with respect to the spherical coordinate system.
4. The method according to claim 3 , wherein the spherical coordinate system is the celestial coordinate system and wherein the orthogonal telescope axes define an alt-azimuth mount configuration.
5. The method according to claim 4 , wherein the position reference indicators comprise encoders coupled to their respective axes, each encoder defining a displacement of the telescope about its respective axis, the displacement based on the respective first and second reference values.
6. The method according to claim 5 , wherein the first terrestrial reference position is a determinable angle with respect to North and wherein the second terrestrial reference position is a determinable angle with respect to horizontal.
7. The method according to claim 6 , wherein the geographic input is a latitude and longitude of the telescope location.
8. The method according to claim 7 , wherein the rotation metric is a time of day.
9. The method according to claim 8 , further comprising:
coupling a global positioning system receiver to the central control processor; and
receiving the geographic input and the rotation metric from the global positioning system receiver.