fig1 illustrates prior art multiple element beam former . such systems are characterized by having at least two active or radiating antenna elements 100 - 1 , 100 - 2 that have associated omni - directional radiating patterns 101 - 1 , 101 - 2 , respectively . the antenna elements 100 are each connected to a corresponding radio receiver , such as down - converters 110 - 1 and 110 - 2 , which provide baseband signals to a respective pair of analog - to - digital ( a / d ) converters 120 - 1 , 120 - 2 . the digital received signals are fed to a digital signal processor 130 . the digital signal processor 130 then performs baseband beam forming algorithms , such as combining the signals received from the antenna elements 100 with complex magnitude and phase weighting functions . one difficulty with this type of system is that performance is heavily influenced by the spatial separation and geometry of the antenna elements 100 . for example , if the antenna elements 100 are spaced too close together , then performance of the beam forming operation is reduced . furthermore , the antenna elements 100 themselves must typically have a geometry that is of an appropriate type to provide not only the desired omni - directional pattern but also operate within the geometry for the desired wavelengths . thus , this architecture is generally not of desirable use in compact , hand held wireless electronic devices , such as cellular telephones and / or low cost wireless access points or stations ( sometimes referred to as a client device or station device ), where it is difficult to obtain sufficient spacing between the elements 100 or to manufacture antenna geometries at low cost . in contrast to this , one aspect of the present invention is to form directional multiple fixed antenna beams , such as a semi - omni or so called “ peanut ” pattern in a very small space . specifically , referring to fig2 , there is the same pair of active antenna elements 100 - 1 , 100 - 2 as in the prior art of fig1 ; however , according to the principles of the present invention , a passive or beam control antenna element 115 is inserted between the active antenna elements 100 . in a receive mode , received signals are fed to the corresponding pair of down converters 110 - 1 , 110 - 2 , a / d converters 120 - 1 , 120 - 2 , and digital signal processor ( dsp ) 130 , as in the prior art . with this arrangement , two beams 180 - 1 , 180 - 2 may be formed simultaneously in opposite directions when the beam control antenna element 115 is switched or fed to a first terminating reactance 150 - 1 . the first terminating reactance 150 - 1 is specifically selected to cause the beam control antenna element 115 to act as a reflector in this mode . since these two patterns 180 - 1 , 180 - 2 cover approximately one - half of a hemisphere , they are likely to provide sufficient directivity performance for a useable antenna system . in an optional configuration , if different antenna patterns are required , such as a “ peanut ” pattern 190 illustrated by the dashed line , then a multiple element switch 170 can be utilized to electrically connect a second terminating reactance 150 - 2 with the beam control antenna element 115 . the multiple element switch 170 may be used to select among multiple reactances 150 to achieve a combination of the different patterns , resulting in one or more “ peanut ” patterns 190 . thus , it is seen how the center beam control antenna element 115 can be connected either to a fixed reactance or switched into different reactances to generate different antenna patterns 180 , 190 at minimal cost . in the preferred embodiment , at least three antenna elements , including the two active antenna elements 100 and single passive element 115 , are disposed in a line such that they remain aligned in parallel . however , it should be understood that in certain embodiments they may be arranged at various angles with respect to one another . various other numbers and configurations of the antenna elements 100 , switch 170 , and passive beam control antenna element ( s ) 115 are possible . for example , multiple active antenna elements 100 ( e . g ., sixteen ) may be used with four passive beam control antenna elements 115 interspersed among the active antenna elements 100 , where each passive beam control antenna element 115 is electromagnetically coupled to a subset of the active antenna elements 100 , where a subset may be as few as two or as many as sixteen , in the example embodiment . another embodiment of an antenna assembly according to the principles of the present invention is now discussed in reference to an antenna assembly 300 depicted in fig3 . the antenna assembly 300 uses a reflector or beam control antenna element 305 , or multiple reflector antenna elements ( not shown ), and a phased array of active antenna elements 310 . the antenna elements 305 , 310 are , in this embodiment , mechanically disposed on a ground plane 315 . the reflector antenna element 305 is used to create its own multi - path . this multi - path is simple and is inside the active antenna elements 310 . because of the close proximity of the reflector antenna element 305 to the active antenna elements 310 , its presence overrides other multi - paths and remove the nulls created by them . the new multi - path has a predictable property and is thus controllable . the phased array can be used to focus its beam on a signal , and the combination of reflector antenna element 305 and active antenna elements 310 removes fading and signal path misalignment , which creates “ ghosts ” often seen in tv receptions . in this embodiment , the reflector 305 is cylindrical and is situated in the center of the circular array 300 of active antenna elements 310 . this distance between the active antenna elements 310 and the conducting surface of the reflector antenna elements 305 may be kept at a quarter wave length or less . the presence of the cylindrical reflector antenna element 305 prevents any wave from propagating through the array 300 of active antenna elements 310 . it thus prevents the formation of standing waves created by the interfering effect of oppositely traveling waves 405 , as indicated by the arrows 415 in fig4 a . the result is that the indoor nulls 410 are removed from the vicinity of the array elements 310 . however , the beam control antenna element 305 creates its own standing waves , as depicted in fig4 b . referring now to fig4 b , the traveling wave 405 travels toward ( i . e ., arrow 415 ) a reflector 420 . the reflector 420 forms a node 410 at the reflector 420 and standing wave 405 having a peak at the antenna elements 310 surrounding the reflector antenna element 305 as a result of the quarter wave spacing . so , with this arrangement , the nulls from the environment are removed , and , at the same time , this arrangement confines the signal peaks to the active antenna elements 310 , which are ready to be phased into a beam that points to the strongest signal path , as determined by a processor ( e . g ., fig2 , dsp 130 ) coupled to the antenna array 300 . fig5 is a top view of example antenna beam patterns 500 formed by the linear antenna assembly of fig2 . in this embodiment , the beam control antenna element 115 is electrically connected to reactance components ( e . g ., fig2 , reactance components 150 - 1 , 150 - 2 ) that creates respective effective reflective rings 505 - 1 , 505 - 2 . for example , the more inductance , the smaller the effective diameter of the ring 505 about the beam control antenna element 115 . responsively , the antenna beam patterns 510 , 515 produced by the antenna assembly 500 , arranged in a linear array , are kidney shaped , as depicted by dash lines . as should be understood , the smaller the diameter of the reflection rings 505 , the narrower the beam and , consequently , more gain , that is provided to the active antenna elements 100 in a perpendicular direction to the axis of the linear array . note that the uncoupled antenna beam patterns 510 , 515 do not form a “ peanut ” pattern as in fig2 , which is caused in part by the selection of the reactance components 150 . a secondary advantage of having this active / beam control / active antenna element arrangement is that the beam control antenna element 115 tends to isolate the two active antenna elements 100 , so there is a potential to reduce the size of the array . it should be understood that the active antenna elements 100 may be spaced closer to one another or farther apart from one another , depending on the application . further , the reflective antenna element 115 electromagnetically disposed between the active antenna elements 100 reduces losses due to mutual coupling . however , loading on the beam control antenna element 115 may make it directive instead of reflective , which increases coupling between the active antenna elements 100 and coupling losses due to same . so , there is a range of reactances that can be applied to the beam control antenna element 115 that is appropriate for certain applications . continuing to refer to fig5 , there are two basic modes of operation of the antenna array : ( 1 ) dual beam high gain ( i . e ., non - omnidirectional ) mode , where the beam control antenna element 115 is reflective and ( 2 ) dual near - omni mode with low mutual coupling , where the center antenna element 115 is short enough but not too short so each active antenna element 100 sees the kidney - shaped beam 510 , 515 , as shown . the reason this is near - omni is because the antenna array is not circular , so it is not a true omni - directional mode . as discussed above , changing the reactance electrically connected to the beam control antenna element 115 changes the mode of operation of the antenna array 500 . examples of the reactances that may be applied to this center passive antenna element 115 are between about − 500 ohms and 500 ohms . also the height of the active antenna elements 100 may be about 1 . 2 inches , and the height of the passive antenna element 115 may be about 1 . 45 inches at an operating frequency of 2 . 4 ghz . it should be understood that these reactances and dimensions are merely exemplary and can be changed by proportionate or disproportionate scale factors . fig6 is a mechanical diagram of a circular antenna assembly 600 . the circular antenna assembly 600 includes a subset of active antenna elements 610 a separated by multiple beam control antenna elements 605 from another subset of active antenna elements 610 b . the active antenna elements 610 a , 610 b , form a circular array . the beam control antenna elements 605 form a linear array . the beam control antenna elements 605 are electrically connected to reactance elements ( not shown ). each of the beam control antenna elements 605 may be selectably connected to respective reactance elements through switches , where the respective reactance elements may include sets of the same range of reactance or reactance values so as to increase the dimensions of a rectangular - shaped reflector 620 , which surrounds the beam control antenna elements 605 , by the same amount along the length of the beam control antenna elements 605 . by changing the dimensions of the rectangular reflector 620 , the shape of the beams produced by the active antenna elements 610 a , 610 b can be altered , and secondarily , the mutual coupling between the active antenna element 610 a , 610 b can be increased or decreased for a given application . it should be understood that more or fewer beam control antenna elements 605 can be employed for use in different applications depending on shapes of beam patterns or mutual coupling between active antenna element 610 a , 610 b desired . for example , instead of a linear array of beam control antenna elements 605 , the array may be circular or rectangular in shape . fig7 is another embodiment of an antenna system 700 that includes an antenna assembly 702 with a beam control antenna element 705 and multiple active antenna elements 710 disposed on a reflective surface 707 in a circular arrangement and electromagnetically coupled to at least one beam control antenna element 705 . as discussed above , the beam control antenna element 705 is electrically connected to an reactance or reactance , such as an inductor 750 a , delay line 750 b , or capacitor 750 c , which are electrically connected to a ground . other embodiments may include a lumped reactance , such as a ( i ) capacitor and inductor or ( ii ) variable reactance element that is set through the use of digital control lines . the reactive elements 750 , in this embodiment , are connected to feed line 715 via a single - pole , multiple - throw switch 745 . the feed line 715 connects the beam control antenna element 705 to the switch 745 . a control line 765 is connected to the ground 755 or a separate signal return through a coil 760 that is magnetically connected to the switch 745 . activation of the coil 760 causes the switch to connect the beam control antenna element 705 to ground 755 through a selected reactance element 750 . in this embodiment , the switch 745 is shown as a mechanical switch . in other embodiments , the switch 745 may be a solid state switch or other type of switch with a different form of control input , such as optical control . the switch 745 and reactance elements 750 may be provided in a various forms , such as hybrid circuit 740 , application specific integrated circuit ( asic ) 740 , or discrete elements on a circuit board . a processor 770 may sequence outputs from the antenna array 702 to determine a direction that maximizes a signal - to - noise ratio ( snr ), for example , or maximizes another beam direction related metric . in this way , the antenna assembly 702 may provide more signal capacity than without the processor 770 . with the mimo 735 , the antenna system 700 can look at all sectors at all times and add up the result , which is a form of a diversity antenna with more than two antenna elements . the use of the mimo 735 , therefore , provides much increase in information throughput . for example , instead of only receiving a signal through the antenna beam in a primary direction , the mimo 735 can simultaneously transmit or receive a primary signal and multi - path signal . without being able to look at all sectors at all times , the added signal strength from the multi - path direction is lost . fig8 a is a diagram of an example use in which the directive antenna array 502 a may be employed . in this example , a station 800 a in an 802 . 11 network , for example , or a subscriber unit in a cdma network , for example , may include a portable digital system 820 such as a personal computer , personal digital assist ( pda ), or cellular telephone that uses a directive antenna assembly 502 . the directive antenna assembly 502 may include multiple active antenna elements 805 and a beam control antenna element 806 electromagnetically coupled to the active antenna elements 805 . the directive antenna assembly 502 a may be connected to the portable digital system 820 via a universal system bus ( usb ) port 815 . in another embodiment , a station 800 b of fig8 b includes a pcmcia card 825 that includes a directive antenna assembly 502 b on the card 825 . the pcmcia card 825 is installed in the portable digital device 820 . it should be understood that the antenna assembly 502 in either implementation of fig8 a or 8 b may be deployed in an access point ( ap ) in an 802 . 11 network or base station in a wireless cellular network . further , the principles of the present invention may also be employed for use in other types of networks , such as a bluetooth network and the like . fig9 - 11 represent an antenna assembly 900 and associated simulated antenna beam patterns produced thereby . referring first to fig9 , the antenna assembly 900 includes four active antenna elements 910 deployed along a perimeter of a circle and a central beam control antenna element 905 . the antenna elements 905 , 910 are mechanically connected to a ground plane 915 . in this embodiment , the active antenna elements 910 have dimensions 0 . 25 ″ to 3 . 0 ″ w × 0 . 5 ″ to 3 . 0 ″ h , which are optimized for the 2 . 4 ghz ism band ( 802 . 11b ). the beam control antenna element 905 has dimensions 0 . 2 ″ w × 1 . 45 ″ h . the height of the beam control antenna element 905 is longer in this embodiment to provide more reflectance and is not as wide to reduce directional characteristics . fig1 a - 10d are simulated beam patterns for the antenna assembly 900 of fig9 . the antenna assembly 900 has been redrawn with x , y , and z axes as shown in fig1 e . the simulated beam patterns of fig1 a - 10d are for individual active antenna elements 910 . the simulation is for 802 . 11b with a carrier frequency of 2 . 45 ghz . the beam patterns are shown for azimuth ( x - y plane ) at phi = 0 degs to 360 degs and elevation = 30 degrees , or theta = 60 degrees . the simulated beam pattern of fig1 a corresponds to the active antenna element 910 that lies along the + x axis . the null in the 180 degree direction represents the interaction between the active antenna element 910 and the beam control antenna element 905 . similarly , the simulated beam pattern of fig1 b corresponds to the active antenna element that lies along the + y axis ; the simulated beam pattern of fig1 c corresponds to the active antenna element 910 that lies along the − x axis ; and the simulated beam pattern of fig1 d corresponds to the active antenna element 910 that lies along the − y axis . the nulls in simulated beam patterns of fig1 b - 10d correspond to the respective active antenna elements 910 and beam control antenna element 905 interactions . referring now to fig1 a - 11c , these simulated antenna directivity ( i . e ., beam ) patterns correspond to the antenna beams produced by the active antenna 910 in the antenna assembly 900 that lies along the + x axis . each of fig1 a - 11c have three antenna directivity curves for theta = 30 , 60 , and 90 degrees , where the angles are degrees from zenith ( i . e , zero degrees points along the + z axis . the simulations of fig1 a - 11c are for 2 . 50 , 2 . 45 , and 2 . 40 ghz , respectively . fig1 d - 11f are simulated antenna directivity patterns for the elevation direction corresponding to the simulated antenna directivity ( i . e ., beam ) patterns of fig1 a - 11c . the three curves correspond to phi = 0 , 45 , and 90 degrees , where the angles are degrees from zenith . fig1 a - 12c are three - dimensional plots corresponding to the cumulative plots of fig1 a - 11f . while this invention has been particularly shown and described with references to preferred embodiments thereof , it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the scope of the invention encompassed by the appended claims .