System and method for controlling an unmanned air vehicle
First Claim
1. A geodetic measuring system comprising:
- a stationary, ground-based geodetic measuring instrument embodied as a total station, a theodolite, or an industrial laser tracker, comprising;
a base;
a support rotatable by motor relative to the base about a vertical axis;
a beam source for emitting a substantially collimated optical beam;
a sighting unit pivotable by motor relative to the support about a horizontal axis;
angle measurement sensors for determining the alignment of the support with respect to the base, and the sighting unit with respect to the support; and
a distance meter using the optical beam;
wherein the support and the sighting unit are configured for aligning an emission direction of the optical beam;
a helicopter-like self-propelled, unmanned aerial vehicle movable in a controlled fashion and positionable at a substantially fixed position, comprising;
an optical module embodied as a reflector for reflecting the optical beam, wherein a distance from the measuring instrument to the optical module can be determined by the distance meter, and an actual position of the aerial vehicle can be continuously derived from the distance and the emission direction of the beam;
a sensor unit having an accelerometer configured to detect inertia values, and a magnetometer configured to detect geographic alignment;
an evaluation unit for determining an actual state of the aerial vehicle in a coordinate system from an interaction of the optical beam with the optical module and the sensor unit, wherein the actual state is defined by the actual position and the geographic alignment, and optionally also a change in position; and
a control unit configured in such a way that, on the basis of an algorithm depending on the actual state and a defined intended state, control data for controlling the aerial vehicle is produced, by which the aerial vehicle is brought into the intended state.
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Accused Products
Abstract
A geodetic measuring system having a geodetic measuring unit having a beam source for emitting a substantially collimated optical beam. The measuring system also has an automotive, unmanned, controllable air vehicle having an optical module. An evaluation unit is also provided, wherein the evaluation unit is configured in such a manner that an actual state of the air vehicle, as determined by a position, an orientation and/or a change in position, can be determined in a coordinate system from interaction between the optical beam and the optical module. The measuring system has a control unit for controlling the air vehicle, wherein the control unit is configured in such a manner that control data can be produced using an algorithm on the basis of the actual state, which can be continuously determined in particular, and a defined desired state, and the air vehicle can be automatically changed to the desired state.
20 Citations
35 Claims
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1. A geodetic measuring system comprising:
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a stationary, ground-based geodetic measuring instrument embodied as a total station, a theodolite, or an industrial laser tracker, comprising; a base; a support rotatable by motor relative to the base about a vertical axis; a beam source for emitting a substantially collimated optical beam; a sighting unit pivotable by motor relative to the support about a horizontal axis; angle measurement sensors for determining the alignment of the support with respect to the base, and the sighting unit with respect to the support; and a distance meter using the optical beam; wherein the support and the sighting unit are configured for aligning an emission direction of the optical beam; a helicopter-like self-propelled, unmanned aerial vehicle movable in a controlled fashion and positionable at a substantially fixed position, comprising; an optical module embodied as a reflector for reflecting the optical beam, wherein a distance from the measuring instrument to the optical module can be determined by the distance meter, and an actual position of the aerial vehicle can be continuously derived from the distance and the emission direction of the beam; a sensor unit having an accelerometer configured to detect inertia values, and a magnetometer configured to detect geographic alignment; an evaluation unit for determining an actual state of the aerial vehicle in a coordinate system from an interaction of the optical beam with the optical module and the sensor unit, wherein the actual state is defined by the actual position and the geographic alignment, and optionally also a change in position; and a control unit configured in such a way that, on the basis of an algorithm depending on the actual state and a defined intended state, control data for controlling the aerial vehicle is produced, by which the aerial vehicle is brought into the intended state. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31)
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32. A geodetic measuring system comprising:
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a stationary, ground-based geodetic measuring instrument embodied as a total station, a theodolite, or an industrial laser tracker, comprising; a base; a support rotatable by motor relative to the base about a vertical axis; a beam source for emitting a substantially collimated optical beam; a sighting unit pivotable by motor relative to the support about a horizontal axis; and angle measurement sensors for determining the alignment of the support with respect to the base, and the sighting unit with respect to the support; and a distance meter using the optical beam; wherein the support and the sighting unit are configured for aligning an emission direction of the optical beam; a helicopter-like self-propelled, unmanned aerial vehicle movable in a controlled fashion and positionable at a substantially fixed position; and an evaluation unit, wherein the evaluation unit is configured in such a way that it is possible to determine an actual state of the aerial vehicle in a coordinate system, determined by a position, an alignment and a change in position, from an interaction of the optical beam with the optical module; and wherein the measuring system comprises a control unit for controlling the aerial vehicle, wherein the control unit is configured in such a way that, on the basis of an algorithm depending on the actual state and a defined intended state, control data can be produced and the aerial vehicle can be brought into the intended state, wherein the optical module is embodied by a reflector which specifies the actual position of the aerial vehicle and the beam can be reflected by means of the reflector, wherein a distance from the measuring instrument to the aerial vehicle is determined by the reflection of the beam and reception at the measuring instrument and the actual position of the aerial vehicle is derived continuously from the distance and the emission direction of the beam, wherein the aerial vehicle has a sensor for continuously measuring an object distance to an object, wherein; the object distance is taken into account when controlling the aerial vehicle; and
/orthe aerial vehicle is controlled in such a way that the aerial vehicle is guided constantly at a specific intended distance from the object depending on the measurement of the object distance. - View Dependent Claims (33, 34, 35)
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Specification