EP0459616A2 - Flugzeugantenne mit Korrektur von Fehlern, verursacht durch die konische Form des Antennenstrahls und durch Flugzeugschräglage - Google Patents

Flugzeugantenne mit Korrektur von Fehlern, verursacht durch die konische Form des Antennenstrahls und durch Flugzeugschräglage Download PDF

Info

Publication number
EP0459616A2
EP0459616A2 EP91303352A EP91303352A EP0459616A2 EP 0459616 A2 EP0459616 A2 EP 0459616A2 EP 91303352 A EP91303352 A EP 91303352A EP 91303352 A EP91303352 A EP 91303352A EP 0459616 A2 EP0459616 A2 EP 0459616A2
Authority
EP
European Patent Office
Prior art keywords
antenna
array
elements
antennas
coupling
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP91303352A
Other languages
English (en)
French (fr)
Other versions
EP0459616B1 (de
EP0459616A3 (en
Inventor
Peter W. Hannan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems Aerospace Inc
Original Assignee
Hazeltine Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hazeltine Corp filed Critical Hazeltine Corp
Publication of EP0459616A2 publication Critical patent/EP0459616A2/de
Publication of EP0459616A3 publication Critical patent/EP0459616A3/en
Application granted granted Critical
Publication of EP0459616B1 publication Critical patent/EP0459616B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/282—Modifying the aerodynamic properties of the vehicle, e.g. projecting type aerials
    • H01Q1/283—Blade, stub antennas
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/08—Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a rectilinear path
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/24—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching

Definitions

  • the Present invention relates to array antennas and multiple array systems for radiating and receiving electromagnetic signals and, in particular, to antennas adapted for use on aircraft which permit the antenna beam to be steered in azimuth or tilted, or both.
  • Identification Friend or Foe (IFF) systems are used to enable aircraft to transmit and receive signals for identification of other aircraft.
  • Airborne radar systems are also used for target location without identification capabilities. The higher frequencies typically used for airborne radar permit use of antennas providing reasonable beam resolution both vertically and horizontally.
  • Airborne linear array antennas used for IFF may, by contrast, lack the capability of providing significant vertical resolution. Without vertical, or elevation, resolving capability, no elevation information is provided by the system.
  • the straight vertical fan beam that the antenna provides in the on-boresight direction perpendicular to the linear array becomes curved or conical in shape when the beam is scanned off boresight. As a result, as illustrated in Fig.
  • the IFF display would accurately indicate a target at 15° right. If however, a target were at location (b) (again 15° right, but at a higher altitude) the IFF display would indicate a target at azimuth (c), displaced from the actual 15° position of the target.
  • the error is introduced by a "coning" of the antenna beam as it is scanned to the right and effectively assumes a profile of a form shown by curved line (d).
  • the resulting errors introduced by off-boresight coning of the IFF beam in addition to affecting the accuracy of the IFF target display, can introduce a displacement between the IFF and radar returns displayed for the same target.
  • a switchable array antenna with a plurality of antenna elements arranged for excitation in subsets of at least three elements, includes terminal means for coupling signals and a plurality of antenna elements each comprising a linear array of at least four elements arranged for use in subsets each having first, second and third elements.
  • First excitation means coupled to the terminal means, includes signal transmission means for coupling forward and rear element signal components of predetermined relative phase and amplitude to first and third elements by way of a point of common voltage.
  • Second excitation means coupled to the terminal means, includes means for coupling to a second element a middle element signal component of predetermined phase and amplitude relative to signal components coupled to the first and third elements.
  • the antenna also includes shifting means for selectively coupling the first and second excitation means to subsets of said antenna elements so that forward, middle and rear signal components can be respectively shifted to different first, second and third element subsets of the plurality of antenna elements.
  • a steerable antenna array system includes a plurality of switchable array antennas spaced laterally in relation to a first radiation direction, each such array antenna comprising a linear array of antenna elements, excitation means for coupling signal components of predetermined relative phase and amplitude to selected antenna elements, and shifting means coupled to said excitation means for altering the coupling of signal components to the antenna elements so as to selectively shift the effective radiation center of each array antenna along its length.
  • the antenna system also includes azimuth control means, coupled to said array antennas, for selectively controlling the shifting means of respective antennas.
  • a beam tilt antenna array system includes terminal means for coupling signals, a plurality of switchable array antennas such as described above and beam tilt control means for coupling a selected plurality of the array antennas to the terminal means.
  • a beam tilt antenna array system may additionally include azimuth control means, coupled to the array antennas, for selectively controlling the shifting means of the antennas, whereby the antenna beam of the antenna system can be independently steered in azimuth and tilted.
  • Fig. 1 illustrates the effect of scanning a linear array antenna off axis.
  • Figs. 2a, 2b, and 2c show orthogonal and simplified exploded views of a low-profile array antenna containing three antenna elements.
  • Fig. 3 shows an array antenna system including five Fig. 2 array antennas.
  • Fig. 4 is a block diagram of an array antenna containing three antenna elements.
  • Fig. 5 shows desirable current relationships for an end-fire array.
  • Fig. 6 is a circuit diagram of a three monopole array antenna.
  • Figs. 7 and 8 are circuit diagrams of alternative forms of the Fig. 6 antenna.
  • Fig. 9 is an antenna pattern for operation of an array antenna of the type shown in fig. 6.
  • Figs. 10a and 10b illustrate component parts of an array antenna of the type shown in Fig. 6.
  • Fig. 11 is a circuit diagram of a three slot array antenna.
  • Figs. 12 and 13 are circuit diagrams of alternative forms of the Fig. 11 antenna.
  • Fig. 14 is a circuit diagram of a five monopole array antenna.
  • Fig. 15 is a circuit diagram of a five monopole switchable array antenna in accordance with the invention.
  • Fig. 16 shows an alternative form of the Fig. 15 antenna utilizing slots.
  • Fig. 17 shows a steerable antenna array system in accordance with the invention.
  • Fig. 18 shows excitation alternatives useful in describing operation of the Fig. 17 antenna system.
  • Fig. 19 shows the straight fan beams that are provided by the Fig. 17 antenna system.
  • Fig. 20 illustrates roll conditions in aircraft banking maneuvers.
  • Fig. 21 shows a steerable beam tilt antenna system in accordance with the inventon.
  • Fig. 22 shows an alternative form of signal distribution network usable with the Fig. 21 antenna system.
  • FIG. 2 there is shown the physical configuration of an array antenna 10 as disclosed in the inventor's copending application entitled “Array Antenna With Forced Excitation,” filed December 19, 1990, Application Number 90313961.6.
  • An understanding of antennas of this type is important to an understanding of the present invention, which provides further improvements in such antennas and systems utilizing them.
  • the present invention is more specifically described under the heading "Description of Figs. 15-22.”
  • Fig. 2a is an orthogonal view of the complete antenna including protective cover 12, of a radiation transmissive material such as fiberglass or a suitable plastic, base member 14, of metal or suitable conductive material to serve as a mounting flange and ground plane connection, and terminal means 16, shown as a coaxial connector suitable for coupling RF signals.
  • protective cover 12 of a radiation transmissive material such as fiberglass or a suitable plastic
  • base member 14 of metal or suitable conductive material to serve as a mounting flange and ground plane connection
  • terminal means 16 shown as a coaxial connector suitable for coupling RF signals.
  • Figs. 2b and c are exploded end and side views, respectively, of the array antenna 10, showing cover 12 and base member 14 with connector 16 attached. Also shown are a first printed circuit card 18 bearing a first planar conductor pattern of forward, middle and rear monopole antenna elements 20, 22 and 24, respectively, and a second printed circuit card 26 bearing a second planar conductor pattern on surface 28.
  • the conductor pattern on surface 28, which is not visible in these views, will be described below.
  • the assembled combination of the cover 12 and base 14 have a height of approximately one-tenth wavelength and length of about three-quarter wavelength.
  • References to dimensions measured in wavelength refer to approximately the average design frequency, so that for a design frequency range or bandwidth of 1,020 to 1,100 MHz, for example, the average design frequency would be 1,060 MHz, corresponding to a wavelength of about 11.1 inches.
  • Dimensions are stated in order to characterize the invention and differentiate over prior art antennas, and are not intended to suggest that the invention is limited to precise dimensions or to exclude antennas representing appropriate applications of the invention. As shown in Fig.
  • the lower surface of base member 14 is flat, but in other embodiments it may be a curved surface corresponding to the curved surface of an aircraft to which it is to be mounted.
  • screws are typically fastened through the mounting holes shown in Fig. 2a and a clearance hole through the outer surface of the aircraft is provided for the connector 16, so that it can be joined to a mating connector for coupling signals to cabling and signal processing equipment carried within the aircraft.
  • Fig. 3 shows a typical antenna system including five array antennas 10a through 10e, supported in a laterally spaced configuration on a curved metal surface 30 such as the fuselage of an aircraft, forward of the pilots' windshield. It will be apparent that in such an installation, use of array antennas one inch in height provides a dramatic improvement in the pilot's visibility, as compared to use of prior art antennas three inches in height. In an installation of this type, the individual array antennas can be excited in groupings selected to provide desired antenna beam characteristics, in accordance with known principles of array antenna excitation.
  • An antenna system as shown in Fig. 3, when installed on the upper forward surface of an aircraft, can provide broad horizontal coverage forward of the aircraft and good vertical coverage, except below the aircraft.
  • a similar antenna system installed on the lower forward surface of the aircraft would permit full vertical and horizontal coverage forward of the aircraft.
  • antenna systems mounted near the leading edge of a wing could provide complete vertical coverage, but would probably require similar systems on the other wing in order to provide complete horizontal coverage free of blockage by the nose of the aircraft.
  • Fig. 4 is a simplified block diagram of an array antenna in accordance with the invention, shown in two sections 18a and 26a corresponding basically to the printed circuit cards 18 and 26 in Fig. 2.
  • the antenna is used to alternatively radiate and receive signals, in the range of 1,020 MHz to 1,100 MHz, which are coupled to and from the antenna by way of the terminal means 16a corresponding to connector 16 in Fig. 2.
  • the cover and base components, 12 and 14, are not represented in Fig. 4.
  • the antenna is used both to radiate and receive signals, and description of how signals are processed by various portions of the antenna when radiating, for example, will be understood to be equally relevant in a reverse relationship during reception.
  • the Fig. 4 antenna includes first, second and third antenna elements 20, 22 and 24, which in accordance with the invention may be monopoles of the order of one-tenth wavelength in height arranged in a spaced linear array. While the desirability of using antenna elements one-tenth wavelength high as compared to prior art elements one-quarter wavelength high may be readily apparent, the severe operational bandwidth degradation normally associated with short antenna elements such as monopoles has been a limiting factor contributing to the continuing reliance on quarter wave elements in the prior art.
  • Section 26a of the Fig. 4 antenna as shown comprises excitation and tuning means which are effective to cause signal currents in the antenna elements 20, 22 and 24 to have a predetermined relationship of phase and amplitude substantially independent of impedance interaction, and are able to accomplish this over a significant band or range of operating frequencies.
  • antenna portion 26a includes first excitation means shown as excitation circuit 40, coupled between terminal 16a and the first and third elements 20 and 24, comprising signal transmission means (as will be discussed in more detail with reference to Fig. 6) for coupling signal components to elements 20 and 24 by way of a point of common voltage, shown as point 42 on the connection between excitation circuit 40 and double tuning circuit 44.
  • Tuning circuit 44 provides double tuning of the impedance characteristics of the antenna ciruits to optimize for operation in a desired frequency range. While circuit 44 is shown as being connected in series between terminal 16a and point 42, its function is to provide wideband impedance matching and it may comprise discrete or distributed reactances coupled to point 42 in series as shown, or in parallel to ground, or may utilize appropriate lengths of transmission line, as will be apparent to those skilled in the art.
  • Section 26a also includes means 46 shown as including second excitation circuit 48, coupled between terminal 16a and second element 22, comprising means for coupling a signal component to the element 22 which has a predetermined phase and amplitude relative to the components coupled to elements 20 and 24 via first excitation means 40. As shown in Fig.
  • excitation circuit 48 functions as a power divider coupling a portion of the input signal from terminal 16a to element 22, while the remaining portion of the input signal flows from the terminal 16a to the other elements.
  • This power divider function of circuit 48 may be provided by a directional coupler (as will be discussed with reference to Fig. 6) or other means.
  • means 46 also includes double tuning circuit 50 for providing double tuning of the impedance characteristics of the middle element 22 for operation in a desired frequency band or range. Where distributed reactances or transmission lines in excitation means 48 are used to provide the double tuning function, means 50 may not appear as a discrete element.
  • Fig. 5 shows a three monopole array arranged to provide an end-fire pattern and Fig, 6 shows such an array antenna with an excitation system in accordance with the invention.
  • a good end-fire pattern is obtainable from the Fig. 5 array if the elements have the spacings and the phase and amplitude of currents shown, Fig.
  • Formd excitation is defined as an excitation arrangement which forces or predetermines the currents in the elements of an array antenna so as to result in currents of desired relative magnitude and phase, substantially independently of mutual and other coupling and impedance effects.
  • first, second and third antenna elements shown as short monopoles 20, 22 and 24 mounted through and above a conductive ground plane 14a.
  • the Fig. 6 array antenna includes first excitation means comprising quarter wave transformer 56 coupled to third monopole 24, and quarter wave transformer 58 arid half wave transmission line 60 coupled to first monopole 20. Transformer 56 and line 60 are also shown coupled to common voltage point 42, as is tuning means 62 which is also coupled to signal input and output terminal 16a.
  • Tuning means 62 is a series resonant LC circuit arranged for double tuning the impedance of rear and forward monopoles 24 and 20.
  • Each of the monopoles is shown as having a series inductance at its base, such as indicator 64 at element 24, for tuning out the capacitive impedances of the short monopole element at one frequency near midband. This narrow band tuning is augmented by the double tuning means 62 to provide substantially increased bandwidth.
  • the Fig. 6 antenna also includes second excitation means comprising a directional coupler 66, for coupling signals of predetermined relative amplitude to the second monopole 22, and second tuning means 68. As shown, coupler 66 is coupled to terminal 16a and is effective to transfer a portion of a signal input to the antenna to monopole 22 by way of transmission line section 70.
  • Second tuning means 68 is a parallel resonant LC circuit arranged for double tuning the impedance of second monopole 22, and the length of line 70 is chosen so that signals reaching monopole 22 have the desired relative phase as compared to signals at monopoles 20 and 24.
  • the two quarter wave transformers 56 and 58 force the currents Ia and Ic in the third and first monopoles 24 and 20 to be dependent substantially wholly on the voltage at the common voltage point 42.
  • the half wave line 60 introduces a reversal in the polarity of Ic at element 20, relative to Ia at element 24.
  • Za + Zc is approximately equal to 15 ohms.
  • the quarterwave transformers and transmission line sections are shown as being sections of microstrip transmission line that are dimensioned to provide the desired characteristic impedances.
  • lines 60 and 70 in this example would be 50 ohm line sections and transformers 56 and 58 would be 27.4 ohm sections one quarter wavelength long at a frequency of 1,060 MHz.
  • Reactive tuning circuits 62 and 68 are used to optimize antenna performance at 1,030 MHz and 1,090 MHz( i.e., are adjusted to double tune the respective antenna elements at those frequencies).
  • Za has negative resistance, making it very difficult to precisely and efficiently provide the desired Ia over a frequency band, in the absence of the invention.
  • (Za + Zc) has a substantial positive resistance which can be efficiently double tuned while providing the desired Ia and Ic values, in accordance with the invention.
  • Achievement of an array antenna pattern with a high front-to-back ratio and strong radiation over a wide angle in the front sector requires precise control of the relative currents in the array elements, as made possible by the present invention.
  • Figs. 7 and 8 there are shown alternative excitation circuits for array antennas similar to the Fig. 6 antenna.
  • the monopoles and the excitation means between point 42 and the monopoles 20 and 24 are the same as shown in Fig. 6.
  • the excitation means for the second element includes a quarter wave transformer 72 similar to transformers 56 and 58 in Fig. 6. Zo of 72 should be different than Zo of 56 and 58.
  • the tuning function can he provided by a series resonant LC circuit 68a and the length of line 70a can be reduced, otherwise operation corresponds to operation of the Fig. 6 antenna.
  • Fig. 7 the tuning function can he provided by a series resonant LC circuit 68a and the length of line 70a can be reduced, otherwise operation corresponds to operation of the Fig. 6 antenna.
  • the excitation means for the forward and rear elements includes a quarter wave transformer 78 similar to transformer 72 included in the second element excitation means in Fig. 7.
  • the parallel resonant LC circuit 62a provides the tuning function, and operation again corresponds to operation of the Fig. 6 antenna.
  • the LC circuits, such as 68a and 62a, may use discrete reactance components or appropriate lengths of transmission line, as will be apparent to those skilled in the art.
  • Fig. 9 is an actual measured azimuth antenna pattern at 1,060 MHz for an array antenna with three monopoles resembling those shown in Fig. 2c, with a monopole width of 2 inches, spacing of 2.78 inches and height of .91 inches, after adjustments for the excitation circuits intended to optimize the results achieved. Note that the front-to-back ratio is greater than 20dB, and the pattern remains strong over a wide angle in the front sector. .Similar results were obtained at 1030 and 1090 MHz. It is believed that the antenna performance reflected in this data is clearly beyond the performance of any known prior art monopole array antenna of comparable dimensions.
  • Figs. 10a and 10b show printed circuit cards 18 and 26 designed for this antenna.
  • three monopoles 20, 22 and 24 as shown were formed by etching a copper layer on dielectric card 18 to leave conductive patterns in the form of the monopoles.
  • the pattern shown on surface 28 of the card 26 was similarly formed.
  • the actual pattern shown on card 26 represents microstip transmission line sections of various lengths and characteristic impedances, together with interconnecting points and sections, desiged to implement the antenna in a physically simple form providing ease of production and assembly, consistent electrical characteristics, inherently high reliability and good durability under shock and vibration conditions common in high-performance aircraft applications. While reference numerals corresponding to the Fig. 6 antenna, with substitution of the alternative excitation circuit of Fig. 8, have been included in Fig.
  • Fig. 11 shows an array antenna in accordance with the invention wherein the individual radiating elements are slots.
  • a three element slot array, as shown, is subject to disruptive mutual coupling effects similar to those previously discussed with reference to monopoles.
  • Slots 80, 82 and 84 in Fig. 11 may simply be openings in a conductive covering 86 on the forward side of a dielectric sheet 88.
  • Conductive covering 86 and dielectric sheet 88 are both shown as being transparent for ease of illustration in order to make visible the other elements which may be disposed on the backside of the dielectric sheet, as shown.
  • Each of the slots or windows 80, 82 and 84 in the conductive member 86 may typically be a half wavelength long or, alternatively, may be shorter with shunt capacitances inserted across the center of the slot at one frequency near midband.
  • the slots in the array are spaced by a quarter wavelength, with a width equal to a fraction of the spacing. Dimensions can be selected for particular applications using known design techniques.
  • each slot is excited by a conductor passing across the slot on the back of the dielectric sheet, as shown at 90, and passing forward or upward through the dielectric 88 to terminate at a point 92 in electrical contact with the conductive covering 86 at the side of slot 80.
  • slot 80 has an excitation conductor termination point 92 at its right side and will be excited with a phase or a polarity of excitation opposite to that of slot 84, which has such termination point at 96 at its left side.
  • each slot is typically backed by a metallic box or conductive cavity to allow radiation only in the forward or outward direction from each slot. It will be appreciated that an antenna in the form of an array of slots is particularly advantageous for implementation in a configuration flush with the surface of an aircraft. The present invention is readily adaptable to such applications.
  • the Fig. 11 antenna includes first excitation means shown as half-wave transmission lines 98 and 100 coupling the third and first elements 84 and 80 to the terminal means 16a via common voltage point 102.
  • Reactive means 62a is shown coupled between point 102 and terminal 16a for providing double tuning in a desired frequency range.
  • Second excitation means, shown as directional coupler 66a, is coupled between terminal 16a and second element 82, via transmission line section 70a and reactive means shown as LC circuit 68a. Operation of the Fig. 11 antenna is similar to the Fig. 6 antenna.
  • Characteristics of slots permit use of transmission line sections 98 and 100 without provision for quarter wave transformers in providing a common voltage point enabling forcing of the voltages across the slots to have the desired magnitude and phase, substantially independently of mutual and other coupling and impedance effects.
  • the significant signal component that determines the radiation pattern of an array is the slot voltage, in contrast to monopole or dipole radiators which have their currents as the significant signal components. Desired slot voltages for a good end-fire pattern with the Fig. 11 array have phase and amplitude values similar to the monopole currents shown in Fig. 5.
  • the Fig. 11 system can provide this forced excitation together with double tuning for increased bandwidth.
  • Figs. 12 and 13 show alternative embodiments regarding the means connecting points 96 and 92 to point 102 in antennas which otherwise correspond to Fig. 11.
  • the half wave transmission lines 98 and 100 have each been replaced be a series combination of two quarter wave transformers, such as transformers 104 and 106 shown as replacing line 100 between points 92 and 102.
  • This arrangement provides wideband transformation of the slot conductance to a convenient value such as 50 ohms at point 102.
  • half wave lines 98 and 100 have been replaced by a single full wavelength transmission line segment 108 connecting points 96 and 92, and reactive tuning circuit 62a connects to a point 102a in the vicinity of point 96.
  • Variations such as shown in Fig. 13 can provide flexibility in particular applications.
  • Fig. 14 there is illustrated an embodiment of the invention comprising a linear array of five antenna elements shown as monopoles 20a through 24a.
  • the first, second and third elements 20a, 22a and 24a (corresponding to the first, second and third elements of Fig. 6) have been supplemented by a leading element 21a, ahead of element 20a, and a trailing element 23a, following element 24a.
  • the arrangement and functioning of elements 20a, 22a and 24a are as described with reference to a three element array, the three element array of first, second and third elements being a basic subset used in antennas utilizing the invention.
  • elements 20a, 22a and 24a correspond to elements 20, 22 and 24 of Fig. 6.
  • the Fig. 14 excitation system corresponds to the alternative excitation system of Fig. 9, with modification for excitation of the additional elements 21a and 23a.
  • a first group of non-adjacent antenna elements 20a and 24a are coupled to first excitation means shown as signal transmission means including halfwave transmission line 60 and quarterwave transformers 56 and 58.
  • the remaining elements, middle element 22a, leading element 21a and trailing element 23a are coupled to second excitation means shown as directional coupler 66, transmission line section 70a, quarterwave transformers 72, 73 and 74, and half and full wavelength transmission lines 75 and 76, respectively.
  • .Signals are coupled by the excitation means to elements 20a and 24a by way of common voltage point 42 and to elements 21a, 22a and 23a by way of a second common voltage point 43, permitting forced excitation.
  • the element 21a, transformer 73 and line 76 could be eliminated.
  • any number of elements there are actually two voltage points in accordance with the invention, to which signals are fed.
  • one of these voltage points is a common voltage point for two elements, permitting predetermined magnitudes and phases of current to be provided.
  • the invention makes available two common voltage points, 42 and 43 for example, each connecting to two or more elements.
  • Fig. 15 includes five antenna elements, shown as monopoles 110, 112, 114, 116 and 118, supported above a ground plane 121 in a linear array and arranged for excitation in subsets of three elements. Shifting means, shown as switch 122, selectively connects the subsets of elements (i.e., elements 110, 112, and 114, elements 112, 114 and 116, or elements 114, 116 and 118) to excitation means for coupling signal components from and to the selected elements during reception and transmission of radiated signals.
  • elements i.e., elements 110, 112, and 114, elements 112, 114 and 116, or elements 114, 116 and 118
  • shifting means 122 which may comprise mechanical or electronic individual switching means such as switches 123 and 124, selectively shift the coupling of signal components appearing at terminals 126, 128 and 130 to different first, second and third element subsets of the antenna elements 110, 112, 114, 116 and 118.
  • shifting means 122 in the position illustrated in Fig. 15, forward, middle and rear signal components for achieving an end-fire antenna pattern directed toward the right are respectively coupled to a first element 114, a second element 112 and a third element 110.
  • the effective element radiation center of the array is shifted forward from the vicinity of element 112 to the vicinity of element 116.
  • the switchable array antenna also includes terminal means, first excitation means, second excitation means and tuning means substantially as described above with reference to Figs. 6 and 7.
  • the terminal means is illustrated as terminal 16a for coupling signals to and from the antenna.
  • First excitation means is shown as including a half-wavelength transmission line 60 for coupling a signal component to terminal 130 with a phase reversal, as compared to the signal component coupled to terminal 126, and a set of two quarter wave transformers for coupling such signal components to first and third elements, respectively, of a selected three element subset of the five antenna elements illustrated.
  • the first excitation means utilizes a quarter wave transformer 144 coupling to element 114 and transformer 132 coupling to element 110.
  • Second excitation means is shown as including directional coupler 66 for coupling a signal component of predetermined amplitude to terminal 128 and a quarter wave transformer 138 coupling to element 112, which is the second element of the selected 114, 112, 110 element subset in this example.
  • Tuning means shown as series LC circuit 68a coupled to the first excitation means via common voltage point 42 and series LC circuit 62 coupled to the second excitation means, provide double tuning of the antenna elements.
  • Figs. 6 and 7 The structure and operation generally and as to individual elements of the excitation and tuning means are covered more specifically in the description of Figs. 6 and 7 wherein corresponding reference numerals refer to similar components. It will be seen, however that the functions of three quarterwave transformers (56, 58 and 72 in Fig. 6 with the Fig. 7 modification) are provided in Fig. 15 by quarterwave transformers 132, 134, 136, 138, 140, 142, 144, 146 and 148, which are utilized in sets of three dependent on the operation of switch 122. Alternatively, three quarterwave transformers can be inserted at points 126, 128 and 130, respectively, and the nine quarterwave transformers in Fig. 15 replaced by nine halfwave transmission lines.
  • the operation of the Fig. 15 antenna is basically as described with reference to Fig. 6.
  • first, second and third elements such as elements 114, 112 and 110
  • an end-fire or other desired antenna pattern is achieved.
  • the Fig. 15 antenna differs in permitting the radiation center of the array to be shifted to be in the vicinity of element 112, 114 or 116, depending on whether excitation is applied to a first, second and third element subset 114, 112, 110 or 116, 114, 112 or 118, 116, 114 by action of the shifting means shown as switch 122.
  • Fig. 15 antenna can be constructed as in Fig. 2 with a protective cover and base member similar to elements 12 and 14 in Fig. 2. Also, antennas in accordance with Fig. 15 can be arranged in a laterally spaced array supported on a surface such as the fuselage of an aircraft, as shown in Fig. 3.
  • the radiating element array 120 is shown as comprising five monopoles coupled to points 111, 113, 115, 117 and 119.
  • Fig. 16 shows an alternative form of radiating element array 120a which can be substituted in a modified Fig. 15.
  • array 120a comprises five slots 110a, 112a, 114a, 116a and 118a illustrated as elongated openings in a conductive layer or surface 86 coupled to an insulative layer or member 88.
  • members 86 and 88 are shown as being transparent to show the connection from point 111, in an insulated relationship across slot 110a behind layer 88, and passing through layer 88 to terminate in contact with layer 86 on the left side of the slot at point 150.
  • a relative phase reversal was introduced for the signal component fed to slot 80 by virtue of the feed conductor crossing to a contact point 92 on the right side of slot 80
  • Fig. 16 all contact points are to the left side of the respective slots.
  • a phase reversal is introduced by the half wave line section 60 shown in fig. 15, so that the Fig. 15 and 16 antennas can both use a similar excitation system such as shown in Fig. 15.
  • the quarterwave transformers in Fig. 15 must be replaced by halfwave transmission lines.
  • Fig. 16 alternative form of antenna is basically as described with reference to Fig. 11, with the additional capability of shifting of the effective radiation center dependent upon the selected excitation of first, second and third element subset 114a, 112a, 110a, or subset 116a, 114a, 112a, or subset 118a, 116a or 114a.
  • the array system includes a plurality of switchable array antennas shown as three identical antennas 152a, 152b and 152c, which may be of the type shown in Fig. 15 or 16.
  • the three switchable array antennas are spaced laterally relative to an end-fire radiation direction to the right in the drawing.
  • signals supplied to terminal 154 are coupled to the three antenna terminals 16a, 16b, and 16c, corresponding to terminal 16a in Fig. 15.
  • Fig. 17 signals supplied to terminal 154 are coupled to the three antenna terminals 16a, 16b, and 16c, corresponding to terminal 16a in Fig. 15.
  • signal components will be coupled by the respective excitation means to a selected first, second and third element subset of the five elements 110, 112, 114, 116 and 118, which are represented by dots, such as dot 118.
  • the active element subset in antenna 152a will be elements 114, 112, and 110, which are circled to indicate the active subset.
  • Fig. 17 there is also included azimuth control means shown as switch controller 156 coupled to the respective shifting means (122 in Fig. 15) of each of the antennas via terminals 122a, 122b and 122c.
  • the shifting means 122 of each antenna may be activated to select one of the three different element subsets and controller 152 comprises a control circuit or mechanism for adjusting the shifting means so that the effective radiation center of each antenna is in a selected position.
  • the shifting means are adjusted in this example so that the effective radiation center is in the vicinity of element 112 for antenna 152a, in the vicinity of element 114 for antenna 152b, and in the vicinity of element 116 for antenna 152c.
  • three Fig. 15 antennas laterally spaced as in Fig. 17 and identically excited in an end-fire mode would produce a beam directed to the right in Fig. 17.
  • excitation of the antennas with different centers of radiation as indicated in Fig. 17 would steer the beam to an angle while preserving the straight shape of the fan beam.
  • Fig. 18 is a simplified representation of three spaced array antennas excited in five different modes.
  • the circles identifying the active elements indicate that the three antennas, such as 152a, b and c in Fig. 17, are identically excited with their centers of radiation along the line 158.
  • Line 158 effectively represents the wavefront for this excitation and would result in a beam direction normal to line 158.
  • excitation is as indicated in Fig. 17, resulting in a rotated wavefront line producing a normal beam direction angled to the left of the original beam direction by an angle of 30°, for example, dependent on the actual dimensioning of the antennas.
  • Fig. 18c indicates a wavefront for a beam angled to the right and Fig.
  • Fig. 18d shows a segmented wavefront resulting in a beam direction angled to the right less than the Fig. 18c beam direction.
  • the beam direction in Fig. 18d can be considered to be the mean of partial beams normal to the two wavefronts represented.
  • the actual beam direction for excitation as in Figs. 18d and e can be calculated or measured based on actual dimensions and characteristics of the antennas to be used, the important point being that relative positioning of the effective radiation centers determines the wavefront and beam position. All of the beams resulting from the excitations shown in Fig. 18 preserve the straight shape of the fan beam. This is shown in Fig. 19.
  • Fig. 17 also shows phase shifters 127a and 127b in channels 16a and 16c, respectively.
  • phase shifters can provide two benefits. First, they may be used to reduce the bend in the wavefront of Fig. 18d or 18e while still preserving the beam direction and the straight shape of the fan beam. Second, they may be used to steer the beam to any azimuth angle between or beyond the five angles shown in Fig. 19. In this case the fan beams become curved, but typically much less curved than the prior art case of Fig. 1.
  • a laterally spaced combination of array antennas with effective radiation centers controlled by azimuth control means can have its antenna beam selectively steered.
  • a target which is off-boresight relative to the antenna system need not be off-boresight relative to the active elements in the antenna system.
  • off-boresight errors associated with coning of the beam are reduced, thereby improving the accuracy of the indicated azimuth bearings of targets at varying altitudes relative to the base aircraft.
  • Fig. 20a is a simplified representation of a section of aircraft fuselage with seven array antennas 152a-g mounted on it (for example, seven Fig. 15 antennas seen in end view).
  • the vertical line 159 in Fig. 20a indicates that the vertical axis of the aircraft is not tilted (i.e. the aircraft is not banking).
  • the three central antennas 152c, d and e in Fig. 20a represent an antenna system with adequate performance in the absence of banking, but that during banking the antenna system is tilted, compromising the performance.
  • the invention permits compensation by selection of an operative group of antennas (identified by the bracket) effectively representing a three antenna system (152d, e and f or 152e, f and g) which is level at a particular degree of roll caused by banking.
  • selection of the three indicated antennas results in a fan beam which remains vertically oriented relative to the horizon.
  • the desired beam compensation has actually been accomplished by tilting the fan beam of the antenna system relative to the aircraft on which it is mounted.
  • the antenna array system includes a plurality of array antennas shown as seven antennas 152a-g, which may be the type shown in Fig. 15 or 16.
  • the antennas are arranged to radiate principally in a forward direction (upward, in the drawing) and are spaced laterally, the spacing being such that in the context of an aircraft fuselage the antennas have displacements in a third direction (which is the vertical direction in the Fig. 20a view), due to the curvature of the fuselage.
  • the antennas are basically shown in top view in Fig. 21 and end view in Fig. 20, so that the relative vertical displacements in Fig. 20 are essentially normal to Fig. 2.1.
  • the Fig. 21 antenna system also includes beam tilt control means, shown as beam tilt control means 160, for selectively activating signal distribution means 162 for determining which group of antennas is active during particular roll conditions. Information representing the degree of roll may be supplied to means 160 or sensed by any appropriate means therein. In either case, tilt control means 160 controls electronic or other switching means 162, shown as including a series of switches such as 162a and 162b, to couple signals between terminal 154a and selected group of antennas, such as antennas 152d, 152e and 152f as shown in Fig. 21, corresponding to compensation for the roll condition shown in Fig. 20b.
  • beam tilt control means 160 controls electronic or other switching means 162, shown as including a series of switches such as 162a and 162b, to couple signals between terminal 154a and selected group of antennas, such as antennas 152d, 152e and 152f as shown in Fig. 21, corresponding to compensation for the roll condition shown in Fig. 20b.
  • a beam tilt antenna may also include beam steering as discussed with reference to Fig. 17.
  • switch control 156a functions in the same manner as switch controller 156 in Fig. 17 to selectively control the shifting means of each active antenna.
  • information from tilt control means 160 indicative of which three of antennas 152a-g are activated at a particular time, is used in means 156a to direct shifting means control information to the currently active antennas.
  • individual radiating elements in an array antenna such as 152a are indicated by dots and active elements by circles for ease of illustration and explanation. The actual elements may be monopoles, slots, etc. as shown and described in greater detail with reference to the other drawings, such as Figs. 6, 11, 15 and 16, and the various alternatives already covered.
  • Phase shifters 127a and 127b for additional azimuth beam control are now located below switching means 162.
  • the antenna fan beam is tilted to the right as the aircraft rolls left, and vice versa, to provide a range of compensation as the fan beam would otherwise deviate from its normal reference or vertical orientation.
  • the antenna beam may be steered as described with reference to Figs. 17 and 18, and the beam steering and tilting can be accomplished independently of each other.
  • Fig. 22 is included to indicate that, where desired, alternative forms of signal feed arrangements known in the prior art may be substituted for the switching approach utilized, in place of signal distribution means 162 as shown in Fig. 21.
  • the phase shifters 164a - 164g in combination with the Butler Matrix and feed network smoothly shift the active portions of the array to compensate for aircraft roll.
  • the phase shifters 166a - 166g provide the additional azimuth beam control.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Details Of Aerials (AREA)
EP91303352A 1990-05-29 1991-04-16 Flugzeugantenne mit Korrektur von Fehlern, verursacht durch die konische Form des Antennenstrahls und durch Flugzeugschräglage Expired - Lifetime EP0459616B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US529836 1990-05-25
US52983690A 1990-05-29 1990-05-29

Publications (3)

Publication Number Publication Date
EP0459616A2 true EP0459616A2 (de) 1991-12-04
EP0459616A3 EP0459616A3 (en) 1992-02-26
EP0459616B1 EP0459616B1 (de) 1996-09-11

Family

ID=24111440

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91303352A Expired - Lifetime EP0459616B1 (de) 1990-05-29 1991-04-16 Flugzeugantenne mit Korrektur von Fehlern, verursacht durch die konische Form des Antennenstrahls und durch Flugzeugschräglage

Country Status (6)

Country Link
EP (1) EP0459616B1 (de)
JP (1) JP2997321B2 (de)
KR (1) KR910020965A (de)
CA (1) CA2030600C (de)
DE (1) DE69121970T2 (de)
IL (1) IL97849A (de)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995001662A1 (en) * 1993-07-02 1995-01-12 Hazeltine Corporation Q equalization in dual-element end-fire array antennas
EP0867972A1 (de) * 1997-03-27 1998-09-30 Denso Corporation Aperturantenne und Radarsystem mit einer derartigen Antenne
EP1507312A1 (de) * 2003-08-14 2005-02-16 Siemens Aktiengesellschaft Verfahren zum Betrieb einer Antenneneinheit einer beweglichen Station sowie entsprechende Antenneneinheit
CN113108753A (zh) * 2021-04-13 2021-07-13 中国电子科技集团公司第三十八研究所 展收机构变形测量方法、系统及展收机构
WO2023179391A1 (zh) * 2022-03-21 2023-09-28 华为技术有限公司 一种天线组件及通信设备

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6664938B2 (en) 2002-03-01 2003-12-16 Ems Technologies Canada, Ltd. Pentagonal helical antenna array

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2236289A1 (en) * 1973-07-05 1975-01-31 Commw Scient Ind Res Org Effectively moving radiation source or antenna - built of sequence of elements fed with staggered power variation with time
US4129870A (en) * 1977-09-30 1978-12-12 Tull Aviation Corporation Apparatus for synthesis of scanning beam
DE3315686A1 (de) * 1983-04-29 1984-10-31 Deutsche Bundespost, vertreten durch den Präsidenten des Fernmeldetechnischen Zentralamtes, 6100 Darmstadt Yagi-gruppenstrahler mit sektorfoermigem richtdiagramm
DE3315685A1 (de) * 1983-04-29 1984-10-31 Deutsche Bundespost, vertreten durch den Präsidenten des Fernmeldetechnischen Zentralamtes, 6100 Darmstadt Yagi-gruppenstrahler mit sektorfoermigem richtdiagramm
US4924235A (en) * 1987-02-13 1990-05-08 Mitsubishi Denki Kabushiki Kaisha Holographic radar

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2236289A1 (en) * 1973-07-05 1975-01-31 Commw Scient Ind Res Org Effectively moving radiation source or antenna - built of sequence of elements fed with staggered power variation with time
US4129870A (en) * 1977-09-30 1978-12-12 Tull Aviation Corporation Apparatus for synthesis of scanning beam
DE3315686A1 (de) * 1983-04-29 1984-10-31 Deutsche Bundespost, vertreten durch den Präsidenten des Fernmeldetechnischen Zentralamtes, 6100 Darmstadt Yagi-gruppenstrahler mit sektorfoermigem richtdiagramm
DE3315685A1 (de) * 1983-04-29 1984-10-31 Deutsche Bundespost, vertreten durch den Präsidenten des Fernmeldetechnischen Zentralamtes, 6100 Darmstadt Yagi-gruppenstrahler mit sektorfoermigem richtdiagramm
US4924235A (en) * 1987-02-13 1990-05-08 Mitsubishi Denki Kabushiki Kaisha Holographic radar

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995001662A1 (en) * 1993-07-02 1995-01-12 Hazeltine Corporation Q equalization in dual-element end-fire array antennas
EP0867972A1 (de) * 1997-03-27 1998-09-30 Denso Corporation Aperturantenne und Radarsystem mit einer derartigen Antenne
US5977904A (en) * 1997-03-27 1999-11-02 Denso Corporation Structure of aperture antenna and radar system using same
EP1507312A1 (de) * 2003-08-14 2005-02-16 Siemens Aktiengesellschaft Verfahren zum Betrieb einer Antenneneinheit einer beweglichen Station sowie entsprechende Antenneneinheit
CN113108753A (zh) * 2021-04-13 2021-07-13 中国电子科技集团公司第三十八研究所 展收机构变形测量方法、系统及展收机构
WO2023179391A1 (zh) * 2022-03-21 2023-09-28 华为技术有限公司 一种天线组件及通信设备

Also Published As

Publication number Publication date
DE69121970D1 (de) 1996-10-17
CA2030600C (en) 2000-04-25
KR910020965A (ko) 1991-12-20
JPH04230105A (ja) 1992-08-19
EP0459616B1 (de) 1996-09-11
IL97849A (en) 1994-06-24
JP2997321B2 (ja) 2000-01-11
EP0459616A3 (en) 1992-02-26
DE69121970T2 (de) 1997-04-10
CA2030600A1 (en) 1991-11-26
IL97849A0 (en) 1992-06-21

Similar Documents

Publication Publication Date Title
US5214436A (en) Aircraft antenna with coning and banking correction
US4414550A (en) Low profile circular array antenna and microstrip elements therefor
US4320402A (en) Multiple ring microstrip antenna
US4125839A (en) Dual diagonally fed electric microstrip dipole antennas
US3971032A (en) Dual frequency microstrip antenna structure
US4922263A (en) Plate antenna with double crossed polarizations
US5173715A (en) Antenna with curved dipole elements
US4173019A (en) Microstrip antenna array
US5708444A (en) Multipatch antenna with ease of manufacture and large bandwidth
US4686536A (en) Crossed-drooping dipole antenna
US4675685A (en) Low VSWR, flush-mounted, adaptive array antenna
US7417597B1 (en) GPS antenna systems and methods with vertically-steerable null for interference suppression
US4547776A (en) Loop antenna with improved balanced feed
US4918457A (en) Antenna formed of strip transmission lines with non-conductive coupling
EP0074762B1 (de) Flügelantenne mit zweifach Richtdiagramm
EP0435562B1 (de) Gruppenantenne mit erzwungener Anregung
EP0431764B1 (de) Antenne mit gekrümmten Dipolelementen
JP3169325B2 (ja) アレーアンテナ
EP1061605B1 (de) Breitbandiges Peilantennensystem mit Einzelapertur mit dualer rechts-,linksdrehender Zirkularpolarisation
EP0459616B1 (de) Flugzeugantenne mit Korrektur von Fehlern, verursacht durch die konische Form des Antennenstrahls und durch Flugzeugschräglage
EP0493014A1 (de) Streifenleitungsantenne
US5559523A (en) Layered antenna
EP0542447B1 (de) Ebene Plattenantenne
CN209730170U (zh) 一种方向图可重构天线单元及相控阵
EP0104173B1 (de) Antennensystem zur elektronischen abtastung mit einer linearen gruppe von yagi antennen

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): DE FR GB IT

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): DE FR GB IT

17P Request for examination filed

Effective date: 19920807

17Q First examination report despatched

Effective date: 19940307

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

ITF It: translation for a ep patent filed

Owner name: JACOBACCI & PERANI S.P.A.

REF Corresponds to:

Ref document number: 69121970

Country of ref document: DE

Date of ref document: 19961017

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20040512

Year of fee payment: 14

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20040519

Year of fee payment: 14

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20040601

Year of fee payment: 14

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050416

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050416

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20051101

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20050416

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20051230

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20051230