Abstract: A method, apparatus, article of manufacture, and a memory structure for generating reconfigurable beams is disclosed herein. The apparatus comprises a stationary feed array having a plurality of selectably activatable feed array elements, the feed array having a feed array sensitive axis; a reflector, illuminated by the selectably activatable feed array elements; a first mechanism, coupled to the reflector, for varying a position of the reflector along the feed array axis; wherein a desired beam size of the antenna system is selected by varying the reflector position along the feed array sensitive axis and by selectably activating the feed array elements.

Abstract: An alignment device for aligning an antenna with a satellite. In one embodiment, the device includes a digital compass to provide an azimuth reading of the antenna when the device is removably affixed to the rear surface of the antenna reflector. In another embodiment, the device includes a first digital level that provides an elevation reading of the antenna when the device is affixed to the rear surface of the antenna reflector. Another embodiment includes first and second digital levels that cooperate to emit a skew signal that is indicative of the skew orientation of the antenna when the device is affixed to the antenna. In yet another embodiment, a speaker is provided adjacent to the antenna to receive a series of tones transmitted by a transmitter that is placed adjacent to a television that is attached to a set top a box that is attached to the antenna.

Abstract: A system having a steerable antenna coupled to a temperature-dependent driver. The driver has a shape-memory element fabricated using a shape-memory alloy (SMA) and having the ability to change its shape as a function of temperature. The element is adapted to steer the antenna to improve signal reception and is controlled by a control circuit, which resistively heats the element while using the strength of the electrical signal generated by the antenna in response to a received radio-frequency signal as a feedback signal. The temperature of the element is adjusted to optimize the signal strength. Systems of the invention may enable customer-performed antenna alignment and are relatively simple and inexpensive to implement.

Abstract: A directive antenna having plural antenna elements is arranged in a parasitic antenna array. Frequency selective components are connected to a first subset of the antenna elements. Weighting structures are connected to a second subset of the antenna elements. The first and second subsets of antenna elements may be connected by a space-fed power distribution system to produce independently steerable beams having spectrally separated signals.

Abstract: A microelectromechanical switch (MEMS) beam-steering antenna array is provided. The antenna comprises an active element including a selectively connectable MEMS, and a lattice of beam-forming parasitic elements, each including a selectively connectable MEMS, proximate to the active element. In some aspects, the active element is a dipole radiator having an effective quarter-wavelength odd multiple length at a first plurality of frequencies in response to connecting radiator MEMS. Likewise, the dipole counterpoise has an effective quarter-wavelength odd multiple length at the first plurality of frequencies in response to connecting counterpoise MEMS. Further, each parasitic element has an effective half-wavelength odd multiple length at the first plurality of frequencies in response to connecting their corresponding MEMS. In other aspects, the active element is a monopole and includes a radiator with a radiator MEMS, a counterpoise groundplane, and parasitic elements with MEMSs.

Abstract: An N-element rotational-symmetric array antenna can generate N fixed pencil-beams simultaneously with an omnidirectional beam. An N×N Butler matrix can be used to feed the array antenna, using fewer than N input ports of the Butler matrix to produce the pencil-beams. One or more of the modes generated by the Butler matrix can be individually accessed to produce one or more corresponding omnidirectional beams. The N×N Butler matrix can be driven by a feed network that provides both power dividing and beam-steering, which permits simultaneous generation of the N pencil-beams.

Abstract: A satellite locator system used with a motor home has a parabolic reflector antenna dish, feedhorn and signal converter mounted on a turntable supporting electronic controls and elevation and azimuth motors operable to rotate the turntable and change the elevation of the dish to locate and target a satellite. A plastic dome mounted on a base plate attached to the roof of the motor home encloses the dish, feedhorn, signal converter, turntable, electronic controls, and elevation and azimuth motors. The dome has an inner semi-hemispherical surface located close to the signal converter to improve the signal strength. A remote console wired to the electronic controls is operable to initiate the satellite search and monitor the status of the satellite search.

Abstract: Radio antennas are aligned with each other for the creation of a fixed radio link, by temporarily mounting a powered actuator on an antenna forming one end of the link, the actuator being arranged to adjust the alignment of the antenna, controlling the movement of the actuator over a range of alignments, measuring the variations in the properties of a signal transmitted over the link as the actuator is moved, identifying an optimum actuator position, and locking the actuator in the optimum position. By using a powered antenna, it is possible to control the alignment of several antennas from a single convenient location. Once the antenna has been secured in the selected position the powered actuator may be recovered for use elsewhere.

Abstract: An antenna control system enabling the remote variation of antenna beam tilt. A drive means continuously adjusts phase shifters of a feed distribution network to radiating elements to continuously vary antenna beam tilt. A controller enables the beam tilt of a number of antenna at a site to be remotely varied.

Abstract: Antennas (8a-8d) are disposed within an antenna body (2) of an antenna system in such a manner as to receive UHF band radio waves coming to the main body (2) from a plurality of first, different directions around the main body (2). Combinations of the antennas (8a-8d) makes the antenna system possible to receive UHF band radio waves coming to the main body (2) from a plurality of second, different directions between adjacent ones of the first directions. Switches (26a-26d) disposed within the main body (2) select one of outputs provided by the individual antennas (8a-8d) and their combinations. An antenna controller (64a), a unit separate from the main body (2), supplies a selection control signal to the switches (26a-26d).

Abstract: A variable gain and variable beamwidth antenna including at least first and second generally planar antenna elements and an antenna element orienter for selectably varying the relative physical orientation of the at least first and second generally planar antenna elements, thereby selectably varying the gain and beamwidth of the antenna.

Abstract: An antenna comprising a phased array of quadrifilar helix or other multifilar antenna elements and a time-delaying feed network adapted to feed the elements. The feed network can employ a plurality of coaxial cables that physically bridge a microstrip feed circuitry to feed power signals to the elements. The cables provide an incremental time delay which is related to their physical lengths, such that replacing cables having a first set of lengths with cables having a second set of lengths functions to change the time delay and shift or steer the antenna's main beam. Alternatively, the coaxial cables may be replaced with a programmable signal processor unit adapted to introduce the time delay using signal processing techniques applied to the power signals.

Abstract: An antenna assembly includes at least two active or main radiating omni-directional antenna elements arranged with at least one beam control or passive antenna element used as a reflector. The beam control antenna element(s) may have multiple reactance elements that can electrically terminate it to adjust the input or output beam pattern(s) produced by the combination of the active antenna elements and the beam control antenna element(s). More specifically, the beam control antenna element(s) may be coupled to different terminating reactances to change beam characteristics, such as the directivity and angular beamwidth. Processing may be employed to select which terminating reactance to use. Consequently, the radiator pattern of the antenna can be more easily directed towards a specific target receiver/transmitter, reduce signal-to-noise interference levels, and/or increase gain by using Radio Frequency (RF), Intermediate Frequency (IF), or baseband processing.

Abstract: A thermal control system for directing fluids between a reservoir and a rotatable platform. The system comprises a rotatable platform having an inlet port for receiving a cooling fluid; a reservoir adjacent the platform houses the cooling fluid for transport to the rotatable platform; and a non rotary jointed conduit having a first end immersed in the cooling fluid of the reservoir provides a fluid path for the cooling fluid to the rotatable platform.

Abstract: An aircraft in-flight entertainment system includes a satellite TV receiver, at least one video display connected to the receiver, and a multi-beam antenna on the aircraft for receiving signals from a plurality of satellite TV transponders. The multi-beam antenna may have right-hand circularly polarized (RHCP) and left-hand circularly polarized (LHCP) beams offset from one another by a beam offset angle. The beam offset angle may be less than an angle defined by the spacing of the DBS transponders. The system may also include an antenna steering positioner connected to the multi-beam antenna, and an antenna steering controller for steering the multi-beam antenna based upon received signals from at least one of the RHCP and LHCP beams. The antenna steering controller may comprise a processor for steering the multi-beam antenna based on a selected master one of the RHCP and LHCP beams and slaving the other beam therefrom.

Abstract: A steerable antenna allows transmission of an electromagnetic signal between a fixed feed source or an image thereof and a target moving within an antenna coverage region. The peak gain of the signal beam varies as a function of the target position following a desired signal gain profile. The antenna includes a reflector defining a reflector surface for reflecting the signal between the feed source or its image and the target. The reflector surface defines a focal point, a center point and a normal axis perpendicular to the reflector surface at the center point. The normal axis and the feed axis intersecting the center point and the feed source or its image define a common offset plane. An elevation rotary actuator rotates the reflector about a rotation axis perpendicular to the offset plane adjacent to the center point so that the antenna provides a nominal signal gain profile over the coverage region.

Abstract: A drive mechanism for an antenna array mounted on a moving vehicle. The antenna array is mounted on a disc having two motors which, cooperatively, rotate the disc and rotate a number of antenna elements mounted on the disc. By rotating the antenna elements, the main lobe of the array may be scanned towards a satellite in the elevation plane. To track a moving source from a moving vehicle, one of the motors rotates the disc as a whole, thereby scanning the beam in the azimuth plane. Each antenna element is at an angle to the vertical so that, by rotating the disc to face the direction of the signal source, such as a satellite, a better signal can be obtained.

Abstract: A multi-reflector antenna array capable of simultaneously transmitting and receiving communication signals at Ku-band frequencies is mounted on an exterior surface of an aircraft. The antenna array provides four cassegrain reflector antennas mechanically connected together in a group capable of being simultaneously mechanically scanned. A common support structure fixes the antennas with respect to each other. A drive mechanism and directional azimuth and elevation motors control the position of the array. The aerodynamic drag of the array is minimized using four antennas rather than a single large diameter antenna. Each antenna is positioned on a common horizontal centerline. Two centrally located antennas are positioned between two smaller diameter antennas. The antennas and positioning equipment are both mounted for rotation within a radome. A corporate power combiner/divider is provided to adjust both an amplitude and a phase of each antenna signal.

Abstract: A beam scanning plane antenna is formed by stacking, in order, a system connecting portion, a Rotman lens portion, and a beam scanning antenna portion. The system connecting portion is formed by stacking, in order, a fourth grounding conductor, a sixth dielectric, a connecting substrate and a fifth dielectric. The Rotman lens portion is formed by stacking, in order, a third grounding conductor, a fourth dielectric, a Rotman lens substrate and a third dielectric. The beam scanning antenna portion is formed by stacking, in order, a second grounding conductor, a second dielectric, a power feeding substrate, a first dielectric and a first grounding conductor. A plurality of antenna groups that each include an irradiating element, a power feeding line and a first connecting portion, are formed on the power feeding substrate. The Rotman lens substrate includes a Rotman lens pattern, a second connecting portion and a third connecting portion.

Abstract: A laser pointer and an image sensor are employed as one measuring system, and two measuring systems are arranged such that a laser beam is irradiated in the opposite direction. One laser pointer and one image sensor are arranged on the measuring reference portion, and also One laser pointer and one image sensor are arranged on the measured portion. The parallel displacement &Dgr;X and the inclination &thgr; of the measured portion are calculated separately based on measured results obtained by these two measuring systems.

Abstract: A steerable antenna allows transmission of an electromagnetic signal between a fixed feed source or an image thereof and a target moving within an antenna coverage region. The peak gain of the signal beam varies as a function of the target position following a desired signal gain profile. The antenna includes a reflector defining a reflector surface for reflecting the signal between the feed source or its image and the target. The reflector surface defines a focal point, a center point and a normal axis perpendicular to the reflector surface at the center point. The normal axis and the feed axis intersecting the center point and the feed source or its image define a common offset plane. An elevation rotary actuator rotates the reflector about a rotation axis perpendicular to the offset plane adjacent to the center point so that the antenna provides a nominal signal gain profile over the coverage region.

Abstract: A satellite locator system used with a motor home has a parabolic reflector antenna dish, feedhorn and signal converter mounted on a turntable supporting electronic controls and elevation and azimuth motors operable to rotate the turntable and change the elevation of the dish to locate and target a satellite. A plastic dome mounted on a base plate attached to the roof of the motor home encloses the dish, feedhorn, signal converter, turntable, electronic controls, and elevation and azimuth motors. The dome has an inner semi-hemispherical surface located close to the signal converter to improve the signal strength. A remote console wired to the electronic controls is operable to initiate the satellite search and monitor the status of the satellite search.

Abstract: Systems and devices for mechanically rotating the polarisation of a signal emanating from or being received by an antenna system. The rotation of the polarisation is achieved by mechanically rotating the feed using a non-metallic drive cord or belt connected to a motor which is displaced outside or behind the radiating aperture. For a linear array of multiple antenna elements, each feed for each antenna element is rotated simultaneously and by an equal amount through the use of a drive system common to all the feeds. The drive system is coupled to each feed and to a drive motor. When the motor is activated, the drive system simultaneously rotates each feed by a given amount. By rotating the feed, the polarisation of the signal is correspondingly rotated and compensation for polarisation loss is provided.

Abstract: An antenna and antenna excitation method. The inventive antenna includes a cylindrical array (20) of radiating elements. Each of the elements is mounted at a predetermined substantially transverse angle relative to a longitudinal axis. A circuit (30) is included for providing an electrical potential between at least two of the elements effective to scan a transmit or a receive beam of electromagnetic energy along an elevational axis at least substantially transverse to the longitudinal axis. In the illustrative embodiment, the array includes a stack of the planar, parallel, conductive, ring-shaped radiating elements, each of which is filled with ferroelectric bulk material. A second circuit (70) is included for exciting at least some of the elements to cause the elements to generate a transmit or a receive beam of electromagnetic energy off-axis relative to the longitudinal axis.

Abstract: A device for sending and receiving electromagnetic waves comprises an antenna with a waveguide, a sending card and a receiving card. The sending card and the receiving card each extend essentially from the waveguide, and therefore from the antenna axis, in a plane perpendicular to this axis and between them form an angle greater than 90°.

Abstract: A cylindrical, ray-imaging, electronically steered array antenna, whose radiating array elements are disposed on a cylindrical surface sector above an electrically conductive ground plane that enhances the antenna gain. The conductive ground plane forms an integral part of the antenna, and the required dimensions of this ground plane depend on the array radius, and on the lowest elevation coverage angle from the (possibly tilted) ground plane. The antenna of the present invention is further characterized by a modular design that tailors the required antenna gain and azimuthal directivity through the stacking of identical antenna segments side by side. The antenna design uses the multiple-beam ray focusing property of a microwave lens when feeding a circular ring array, while producing at the same time coherent ray imaging from a bottom metal plate.

Abstract: In one embodiment, an antenna device includes a scanning reflector, a fixed feeder interacting with the reflector for emitting radar radiation and a detector for detecting reflector passage of at least two different predetermined scanning positions during scanning of the reflector. The antenna device also includes a timer used to determine passage times at the time of reflector passage of the scanning positions. The scanning position of the reflector is predicted at an arbitrary time on the basis of the passage times and a predetermined scanning motion of the reflector. In another embodiment, a method for determining an accurate scanning position for the scanning reflector of the antenna device is disclosed.

Abstract: An assembly of mechanically steerable directional radio antennas, comprising a primary antenna and at least one secondary antenna, arranged such that the or each secondary antenna is capable of being physically steered over a limited azimuthal arc relative to the primary antenna, and is at least partially within the swept volume of the primary antenna. By allowing the swept volumes of the antennas to overlap, a compact assembly can be provided, whilst by limiting the azimuthal movement of the secondary antennas relative to the primary, it can be arranged that the antennas do not foul each other.

Abstract: A radar antenna system comprises a wheel, cone or frustum having an axis. The wheel, cone or frustum has a circumferential portion adapted to engage at least one path disposed on a platform for revolving the radar array about the platform. A radar array is mounted on the wheel, cone or frustum, with the axis normal to a face of the radar array. The wheel, cone or frustum rotates about the platform as the radar array revolves around the platform during operation.

Abstract: A steerable antenna or scanner assembly (10) is connected to signal process means (12). A housing (14) surrounds a focusing antenna (16) which is stationary relative to the housing (14), a polarisation rotator (18), a steerable reflector (20) angularly movable about a pivot axis (22), and a detector (24). Incoming radiation passes through the focusing antenna (16), has its polarization altered as it passes through rotator (18), reflects off reflector (20), Passes through rotator (18) again, encounters the antenna (16) again and this time reflects off it to focus down, passes through rotator (18) again, encounters the steerable reflector (20) again and this time passes through it to reach the detector (24). Moving the reflector (20) angularly steers the directional sensitivity of the assembly (10).

Abstract: A method and apparatus are provided for tracking a signal source using an antenna with a predetermined beamwidth. The method includes the steps of measuring a signal level from the signal source along an arc within the beamwidth of the antenna, determining a rate of change of the measured signal level along the arc and solving for a position on the arc where the determined rate of change of the signal level substantially equals zero.

Abstract: A low profile, vehicle mounted, in-motion tracking, satellite antenna includes a pair of antenna assemblies mounted in parallel on a rotatable platform. Each antenna assembly includes two subreflectors with a plastic matching element. The outputs of the two antenna assemblies are coupled with a single phase shifter. The combined outputs are retransmitted to a receiver inside the vehicle. The satellite antenna also includes a receiver for receiving channel selection data and/or for providing two-way communication with equipment inside the vehicle. The antennae, transmitter and receiver are self-powered by a storage device which is charged by a wind driven generator. A retractable radome lowers to a lower profile when the antenna is not in use.

Abstract: A satellite locator system used with a motor home has a parabolic reflector antenna dish, feedhorn and signal converter mounted on a turntable supporting electronic controls and elevation and azimuth motors operable to rotate the turntable and change the elevation of the dish to locate and target a satellite. A plastic dome mounted on a base plate attached to the roof of the motor home encloses the dish, feedhorn, signal converter, turntable, electronic controls, and elevation and azimuth motors. The dome has an inner semi-hemispherical surface located close to the signal converter to improve the signal strength. A remote console wired to the electronic controls is operable to initiate the satellite search and monitor the status of the satellite search.

Abstract: Apparatus for controlling the rotational position of a dipole antenna (10) to compensate for roll and pitch movements of an unmanned air vehicle (UAV). The antenna (10) is connected to a duel-axis roll and pitch antenna mount (26), the rotational position is controlled by a pair of motor position control and feedback circuits (20 and 32). Roll error and pitch error signals (12 and 14) obtained from gyro systems in the UAV are subtractively combined with roll and pitch position signals, to generated control signals to be applied to rotate the antenna mount in a way that compensates for the roll and pitch movements of the UAV, and effectively isolates the antenna mount from roll and pitch movements of the UAV. The dipole antenna (10), therefore, has its radiation pattern and polarization direction aligned with ground-based antennas, thus providing higher gain, increased range and more reliable performance.

Abstract: A position sensing system for a radar array includes a marker located on a portion of an array assembly. The array assembly includes a radar array that rotates about an axis normal to a radiating face of the radar array during operation. An optical sensor detects the marker to sense an angular position of the radar array.

Abstract: An apparatus for determining an instrument boresight azimuth heading is disclosed. A typical apparatus comprises a gyro having a first input and a first output and a rocking angle generator having a second output, wherein the second output is communicatively coupled to the first input of the gyro, producing a demodulated signal at the first output. A signal multiplier is communicatively coupled to the second output and the demodulated signal for multiplying the second output and the demodulated signal and producing a multiplied signal and a filter communicatively coupled to the multiplied signal for producing a filtered output.

Abstract: A method of aligning an antenna within a predetermined azimuth direction, in which the antenna is hingeably connected to a support. In response to processed positioning data received by a first global positioning system receiver dish from a global positioning satellite system, the first receiver dish being connected to the antenna and locatable at predetermined first and second positions away from the antenna, the first receiver dish determines an antenna azimuth direction and is moved from the antenna azimuth direction towards the predetermined azimuth direction so as to align the antenna.

Abstract: A thermal control system for directing fluids between a reservoir and a rotatable platform. The system comprises a rotatable platform having an inlet port for receiving a cooling fluid; a reservoir adjacent the platform houses the cooling fluid for transport to the rotatable platform; and a non rotary jointed conduit having a first end immersed in the cooling fluid of the reservoir provides a fluid path for the cooling fluid to the rotatable platform.

Abstract: A laser pointer and an image sensor are employed as one measuring system, and two measuring systems are arranged such that a laser beam is irradiated in the opposite direction. One laser pointer and one image sensor are arranged on the measuring reference portion, and also One laser pointer and one image sensor are arranged on the measured portion. The parallel displacement &Dgr;X and the inclination &thgr; of the measured portion are calculated separately based on measured results obtained by these two measuring systems.

Abstract: A radar antenna system comprises a wheel, cone or frustum having an axis. The wheel, cone or frustum has a circumferential portion adapted to engage at least one path disposed on a platform for revolving the radar array about the platform. A radar array is mounted on the wheel, cone or frustum, with the axis normal to a face of the radar array. The wheel, cone or frustum rotates about the platform as the radar array revolves around the platform during operation.

Abstract: A position sensing system for a radar array includes a marker located on a portion of an array assembly. The array assembly includes a radar array that rotates about an axis normal to a radiating face of the radar array during operation. An optical sensor detects the marker to sense an angular position of the radar array.

Abstract: An azimuth drive for a radar array comprises at least one circular track mounted to a wheel on which the radar array is mounted. A motor is coupled to the at least one circular track and capable of moving along the track in the tangential direction, to relocate the center of mass of the wheel on which the radar array is mounted.

Abstract: A ground-based antenna for use with a satellite communications (SATCOM) system that reduces interference from geosynchronous earth orbit (GEO) satellites. Because GEO satellites that provide coverage of the continental United States (CONUS) are uniformly separated along an equatorial arc around the earth, the GEO satellites are approximately uniformly separated in sine space when viewed from a ground terminal located within CONUS over typical communications frequency bands, such as the Ka band (29-39 GHz) and the Ku band (10-15 GHz). The invention can reduce interference by providing an uniformly illuminated rectangular aperture, in which the horizontal dimension is chosen so when the aperture is normal to a transmission axis between the antenna and the Nth satellite of a SATCOM systems, the nulls of the antenna radiation pattern align with the N±1, N±2, N±3, . . . satellites.

Abstract: A pod mount assembly 20 is configured in a folding quad pod design with four ground-engaging legs 22, 24, 26, 28, and a rotatable central column 30. The ground-engaging legs rotatably connect to the base of the central column 30. The central column 30 contains a telescoping central shaft 32. The central column 30 is rotatable from a horizontal position into a vertical position. The telescopic shaft 32 is extendable upward from a retracted position within the central column 30 into a extended position there above. The pod mount assembly 20 includes a hydraulic pump and cylinder to rotate the central column 30 and extend the telescopic shaft 32. The unique folding and collapsible design of the pod mount assembly 20 creates a small form factor for high mobility and ease of deployment. The pod mount assembly 20 acts as the mounting base for an antenna assembly 10.

Abstract: The present invention provides a system for avoiding code collisions from multiple SAW identification tags and a method of operating such system. In one embodiment the invention provides for (1) focusing an interrogation pulse to within a defined space; and (2) discriminating between coded responses returned from tags located within such defined space.

Abstract: The elevation angle and azimuth angle and the required angles of rotation for the first antenna 33 and the second antenna 34 are calculated using predetermined calculating means. The elevation adjustment mechanism and azimuth adjustment mechanism and rotating mechanisms of the first antenna 33 and the second antenna 34 are controlled so that the first antenna 33 and the second antenna 34 will be pointed toward respective communication targets T1 and T2 (the first satellite and the second satellite).

Abstract: An antenna system adapted to be mounted on an exterior surface of a mobile platform and having a reduced overall height to reduce aerodynamic drag caused by the antenna system. The antenna system includes a movable platform disposed concentrically within an annular stationary platform. The movable platform includes a slip ring assembly formed on its lower surface which is in physical contact with a brush assembly supported from a lower surface of the stationary platform. By locating the slip ring assembly and the brush assembly adjacent the lower surface of the movable platform, the overall height of the antenna is reduced. Reliability is also improved since contaminants are less likely to accumulate on the slip ring assembly due to its presence on the lower surface of the movable platform.

Abstract: The invention relates to an antenna device comprising a group antenna (310) with radiating elements (340-347) in M rows and N columns M, where N<M, which group antenna (310) has a width measurement (b) and a height measurement (h). The group antenna (310) is so arranged in the antenna device that the projection (P) of the group antenna in the sideways direction of the antenna in the horizontal plane (210) exceeds the width measurement (b) of the group antenna, whereby the group antenna is given a narrower main lobe in the horizontal plane (210).

Abstract: An antenna arrangement includes an antenna reflector (10), a transceiver element (11) and a signal detection unit (12) having a signal converter (121-122) and a computing unit (123) for generating in response to incoming signals control signals for controlling the alignment of the antenna reflector (10) with a target object. The signal converter (121-122) is adapted to reduce its bandwidth automatically and incrementally from a requisite maximum frequency range to a narrow band frequency range. Changes in the direction of the antenna reflector are detected through the medium of a movement detection unit (13) that includes 3d-sensors (131, 132, 133). Mechanical control of the alignment direction of the antenna reflector (10) is effected with the aid of a drive unit (15).

Abstract: In order to provide a reflector antenna apparatus which can be installed within a small space, which has adequate practicality, and which can perform scanning by pivoting about two axes which are perpendicular to each other, in a reflector antenna apparatus having a Cassegrain reflector and a rotating mechanism which rotates the reflector about an azimuth axis and an elevation axis, a reflector with a substantially rectangular aperture has its elevation axis passing through substantially the central portion of the height dimension of the reflector, and reflector surface adjustment is carried out such that substantially all of the electromagnetic waves which are supplied are received and reflected, whereby the antenna height does not become large when the reflector rotates about the elevation axis. The reflector may be an array of a plurality of reflector elements.