SE545208C2

SE545208C2 - Dual-Band Radio Terminal and Filter Structure

Info

Publication number: SE545208C2
Application number: SE2150108A
Authority: SE
Inventors: Anders Ellgardt; Fredrik Holmberg; Fredrik Wester; Kennet Lejnell
Original assignee: Ovzon Sweden Ab
Priority date: 2021-01-29
Filing date: 2021-01-29
Publication date: 2023-05-23
Also published as: SE2150108A1

Abstract

A filter structure (300) has a frame (325) carrying a filter compartment (120T/R) that holds first and second waveguide filters (F1H, F2H; F1L, F2L). The filter compartment (120T/R) is rotatable (R) a predetermined angle around a rotation axis (AV) relative to the frame (325) so as to either engage the first waveguide filter (F1H, F2H) or the second waveguide filter (F1L, F2L) in a waveguide conduit (121; 122), thus rendering the waveguide conduit adapted for forwarding radio-frequency signals at a higher band or a lower band respectively. Consequently, the filter structure (300) is suitable for inclusion in a dual-band radio terminal for communication with spacecrafts via an antenna unit exchanging radio-frequency signals bidirectionally with the spacecrafts.

Description

Dual-Band Radio Terminal and Filter Structure TECHNICAL FIELD The invention relates generally to satellite terminal design. ln particular, the present invention concerns a terminal for dual- band radio communication with spacecrafts. The invention also relates to a filter structure for engaging selectively either a first waveguide filter or a second wave-guide filter in a waveguide conduit, thus rendering the waveguide conduit adapted for for- warding radio-frequency signals at a higher band or a lower band respectively.

BACKGROUND Typically, a satellite terminal for dual band operation is designed such that the user must swap certain key components when switching between the frequency bands. The specific compo- nents necessary to swap varies between different designs and ranges from filters, amplifier circuitry, receiver circuitry and even the antennas, if a common antenna cannot be made wideband enough. ln other words, basically half the terminal may need to be swap- ped in connection with changing bands. This is inconvenient and time consuming, and may lead to malfunction and/or loss of vital pieces of equipment. Moreover, if the terminal is mobile, the user must carry around a number of interchangeable compo- nents. The overall terminal kit therefore becomes relatively volu- minous.

CN 108288764 shows a Ku/Ka switching dual-band feeder net- work and various forms of antennas in wireless microwave satel- lite communications or antennas in electronic reconnaissance signals. The design, which includes a Ku/Ka-band switching mic- rowave network, a Ku-band polarization rotating mechanism, two Ka-band filters and a fixed platform thereby avoids the need for swapping components when switching between the Ku and Ka bands. However, the design is comparatively inefficient with res- pect to the volume occupied.

EP 1344275 discloses a device for filtering electromagnetic wa- ves, which device includes a cylindrical element containing wa- veguide filters that are centered on an axis. Here, different pairs of transmitter/receiver filters are selected by rotating the cylin- drical element, which contacts the source antenna and the transmission/reception block of the transmitter/receiver device.

Although the above designs overcome some of the problems outlined initially, none of these prior-art designs is compact en- ough to provide a truly volume-efficient solution, which is suit- able for integration into a mobile terminal.

SUMMARY One object of the present invention is therefore to offer on im- proved dual-filter structure and a terminal design, which enables a minimized overall size while avoiding any additional compo- nents.

According to one aspect of the invention, the object is achieved by a terminal for dual-band radio communication with space- crafts. The terminal contains: an antenna unit, first and second amplifying and frequency-mixing circuitries and a modulator-de- modulator unit. The antenna unit is configured to exchange ra- dio-frequency signals bidirectionally with the spacecrafts. The first amplifying and frequency-mixing circuitry is configured to up convert an outgoing modulated signal to be fed through a first waveguide conduit connected to the antenna unit. The second amplifying and frequency-mixing circuitry is configured to down convert an incoming signal received through a second wave- guide conduit connected to the antenna unit. The modulator-de- modulator unit is configured to transform an outgoing baseband signal into the outgoing modulated signal and transform an incoming modulated signal down converted from the incoming signal into a received baseband signal. Each of the first and se- cond waveguide conduits is arranged to forward radio-frequency signals on at least two separate bands. Specifically, the first and second waveguide conduits contain a respective or a common filter compartment that is rotatable a predetermined angle around a rotation axis relative to a frame so as to either engage a first waveguide filter pair or a second waveguide filter pair in the first and second waveguide conduits. Here, the first wave- guide filter pair is adapted for radio communication at a higher band than the second waveguide filter pair.

This terminal is advantageous because it enables a low- profile/flat design, which is suitable to be arranged along a flat surface, such as an antenna array, and thus attains a highly volume-efficient solution.

According to embodiments of this aspect of the invention, the fil- ter compartment is rotatable 180 or 90 degrees around the rota- tion axis relative to the frame. The rotation axis, in turn, may either be perpendicular or parallel to a flat surface onto which the frame is mounted.

Rotation 180 degrees around the rotation axis is advantageous, since it allows a very compact design, especially if the rotation axis is perpendicular to the flat surface. Namely, in such a case the first and second waveguide filters may be arranged side by side with a respective lowest side protruding from the flat sur- face.

Rotation 90 degrees around the rotation axis is advantageous, since it requires less movement when switching bands. Further, if the rotation axis is perpendicular to the flat surface, the 90 degrees rotation embodiment accomplishes a maximal distance between the engaged and non-engaged waveguide filters, which, in turn, vouches for small signal leakage.

According to yet another embodiment of this aspect of the in- vention, the filter compartment is configured to be manually ro- tated by a user of the terminal. Hence, the design becomes ro- bust, cost-efficient and light-weight.

According to still another embodiment of this aspect of the in- vention, alternatively or additionally, the terminal contains an el- ectric motor, or other kind of automatically controllable actuator device, which is configured to cause filter compartment to rotate in response to a control signal. Thereby, the terminal may switch frequency bands without involving the user, and even by remote control.

According to another embodiment of this aspect of the invention, the terminal contains a sensor arrangement configured to pro- duce a signal indicating which of the first and second waveguide filter pairs that is engaged in the first and second waveguide conduits. Preferably, the sensor arrangement is further configu- red to indicate if the one of the first or the second waveguide fil- ter pairs being engaged in the first and second waveguide con- duits is properly positioned therein. Consequently, proper and reliable operation of the terminal can be ensured.

According to another aspect of the invention, the object is achie- ved by a filter structure for engaging selectively either a first waveguide filter or a second waveguide filter in a waveguide conduit, thus rendering the waveguide conduit adapted for for- warding radio-frequency signals at a higher band or a lower band respectively. The filter structure contains a frame carrying a filter compartment that, in turn, holds the first and second wa- veguide filters. The filter compartment is rotatable a predeter- mined angle around a rotation axis relative to the frame so as to either engage the first waveguide filter or the second waveguide filter in the waveguide conduit. Hence, a low-profile/ flat design is enabled, which is suitable for volume-efficient arrangement along a flat surface, such as an antenna array.

According to one embodiment of this aspect of the invention, the filter structure contains at least one leakage reduction compo- nent, which is configured to reduce an outflow of signal energy outside of the first or second waveguide filter respectively being engaged in the waveguide conduit. Thereby, the user may con- veniently and efficiently switch between the two frequency bands and maintain a high signal quality at each of said bands when transmitting as well as receiving signals.

According to other embodiments of this aspect of the invention, the at least one leakage reduction is represented by: at least 10 one waveguide choke configured to screen off electromagnetic energy from an input to or an output from the filter structure; at least one stub element arranged in an outer wall of the filter compartment, which at least one stub element is configured to prevent leaking electromagnetic energy from propagating along said outer wall; and/or at least one spring-assisted contact member arranged in a bearing ring of the filter compartment, which at least one contact member is configured to cause galva- nic contact between the filter compartment and the frame thus shortcutting any leaking electromagnetic energy. Hence, com- pact and efficient leakage reduction is attained.

Further advantages, beneficial features and applications of the present invention will be apparent from the following description and the dependent claims.

BRIEF DESCRIPTION OF THE DRAWINGS The invention is now to be explained more closely by means of preferred embodiments, which are disclosed as examples, and with reference to the attached drawings.

Figure 1 shows a block diagram of a terminal according to one embodiment of the invention; Figures 2a, b show frequency graphs illustrating a general concept according to the invention, wherein FigureFigureFigures 5a, b FigureFigures 7,FigureFigures10a,11a Figures10b, 11b signals are transmitted and received via a common antenna unit; illustrates a filter structure according to a first embodiment of the invention; illustrates a filter structure according to a se- cond embodiment of the invention; illustrate a filter structure according to a third embodiment of the invention; illustrates a filter structure according to a fourth embodiment of the invention; illustrate various leakage reduction compo- nents according to embodiments of the inven- tion; illustrates a filter structure according to a fifth embodiment of the invention; show frequency graphs illustrating a first com- bination of a receiver-transmitter pair of filters according to one embodiment of the invention; and show frequency graphs illustrating a second combination of a receiver-transmitter pair of fil- ters according to one embodiment of the in- venüon.

DETAILED DESCRIPTION Figure 1 shows a block diagram of a terminal 100 for dual-band radio communication with spacecrafts according to one embodi- ment of the invention. The terminal 100 contains an antenna unit 110, a first amplifying and frequency-mixing circuitry 130, a se- cond amplifying and frequency-mixing circuitry 150 and a modu- lator-demodulator unit The antenna unit 110 is configured to exchange radio-frequency signals RFR and RFT respectively in a bidirectional manner with the spacecrafts, for example on the AP3OB Ku and the Standard Ku bands. The AP3OB Ku band uses the following terminal fre- quencies for reception:10.7 - 10.95 GHz and 11.2 - 11.45 GHz, and for transmission 12.75 - 13.25 GHz. The Standard Ku band uses the following terminal frequencies for reception: 10.95 - 11.2 GHz and 11.45 - 12.75 GHz, and for transmission 13.75- 14.5 GHz.

The first amplifying and frequency-mixing circuitry 130 is confi- gured to up convert an outgoing modulated signal TX to be fed through a first waveguide conduit 121 connected to the antenna unit 110 in the form of a signal for transmission Tw.

The second amplifying and frequency-mixing circuitry 150 is configured to down convert an incoming signal RW received through a second waveguide conduit 122 connected to the an- tenna unit 110. The incoming signal RW is down converted into an incoming modulated signal RX.

According to embodiments of the invention, either or both of the a first and second waveguide conduits 121 and/or 122 may be implemented by means of transmission lines, e.g. a microstrip, stripline or coaxial cable.

The modulator-demodulator unit 140 is configured to transform an outgoing baseband signal BBT into the outgoing modulated signal TX, and transform the incoming modulated signal RX into a received baseband signal BBR.

Each of the first and second waveguide conduits 121 and 122 respectively is arranged to forward radio-frequency signals on at least two separate bands, which in Figure 1 are denoted Fin/Fn and Fzn/Fzt respectively.

The first and second waveguide conduits 121 and 122 either contain a respective filter compartment, or a common filter com- partment holding waveguide filters for the separate bands F1H/ F1L and Fzn/Fzt, as will be exemplified below with reference to Figure 9. ln Figure 1, a first filter compartment for the transmit- ter filters F1H and F1L is denoted 120T, and a second filter com- partment for the receiver filters F2H and Fzt is denoted 12OR.

As will be described below with reference to Figures 3 to 6, the filter compartment(s) 120T and 12OR is(are) rotatable a prede- termined angle around a rotation axis relative to a frame so as to either engage a first waveguide filter pair F1H and Fzn respec- tively or a second waveguide filter pair Fit and Fzt respectively in the first and second waveguide conduits 121 and 122 respec- tively. Here, the first waveguide filter pair Fin and F2H is adapted for a relatively high frequency band, and the second waveguide filter pair Fn and Fzt is adapted for a relatively low frequency band. Of course, according to the invention, the opposite rela- tionship is equally well conceivable.

Figures 2a and 2b show frequency graphs illustrating a general concept according to the invention, wherein signals are trans- mitted and received via a common antenna unit Figure 2a shows a graph representing a symbolic signal gain |S12| in a linear scale from 0 to 1 along the vertical axis and frequency along the horizontal axis. A right-hand side vertical axis designates spectral signal energy P. The graph in Figure 2a depicts a first frequency response for a first waveguide filter, say F1H, of the transmitter filter 120T having a transmitter pass- band PB(TX) extending from a first frequency f1 and up. The transmitter passband PB(TX) is adapted to let a transmitted sig- nal through with a first spectrum P(TX). Below first frequency f1, the transmitter filter 120T is configured to discriminate/block any transmitted noise energy from the first amplifying and frequency- mixing circuitry 130. Thus, the transmitter filter 120T prevents increase of a noise level of the second amplifying and fre- quency-mixing circuitry 150 in a receiver passband PB(RX) ex- tending up to a second frequency f2 being lower than the first frequency f Figure 2b shows a graph representing a symbolic signal gain |S12| in a |inear scale from 0 to 1 along the vertical axis and frequency along the horizontal axis. Analogous to Figure 2a, a right-hand side vertical axis also designates spectral signal energy P. The graph in Figure 2b depicts a second frequency response for a second waveguide filter, say F2L, of the receiver filter 12OR having the receiver passband PB(RX) extending up to the second frequency f2. This means that, above the second fre- quency f2, the receiver filter 12OR is configured to discriminate/ block any noise energy received from the antenna unit 110 and the signal transmitted from the antenna unit 110. Consequently, Thus, the receiver filter 12OR prevents increase of a noise level of the first amplifying and frequency-mixing circuitry 130 in the transmitter passband PB(TX), which may be reflected back into the antenna unit ln general, filters are designed to let through/transfer signals in frequency bands, so-called passbands, and discriminate/block against signals in so-called stop bands. ln between said pass and stop bands, the filter response continuously changes from the passband to the stop band. The steepness of the change is called the filter's roll off. To improve the roll off of the filter de- sign, the designer needs to add poles of the filter. As a result, a steeper filter generally needs to be larger in size and often have higher losses in the pass band of the filter. To guarantee that adequate performance is achieved by the transmitter and recei- ver filters 120T and 12OR respectively, a guard band is used in between the transmitter passband PB(TX) and the receiver pass- band PB(RX). The guard band allows the filters' roll offs to belo- cated outside of the frequency ranges of the transmitter and re- ceiver passbands PB(TX) and PB(RX) respectively. Thereby, the transmitter and receiver filters 120T and 12OR may function as described above.

The invention allows the terminal 100 to include transmitter and receiver circuitry 130 and 150 to be operable in a larger set of frequency bands than what is possible with a terminal employing traditional filtering. According to the invention, the transmitter passband PB(TX) of the first waveguide conduit 121 may over- lap, or be spectrally very close to the receiver passband PB(RX) of the second waveguide conduit Furthermore, the terminal 100 is configured to enable a change between a first waveguide filter pair F1H/Fm and a second wave- guide filter pair F1L/F2L in the first and second waveguide con- duits 121 and 122 respectively. Thereby, an arbitrary transmitter passband PB(TX) may be used in the transmitter passband PB(TX) or an arbitrary receiver passband PB(RX) in the receiver passband PB(RX). However, the combination of filter pairs F1H! F2H and F1L/F2L must fulfill the requirement that filters pass bands and stop bands coincide with frequencies used as ex- plained above. ln Figure 3, we see a filter structure 300 according to a first em- bodiment of the invention. Here, a first waveguide filter F1H is implemented to the right in a cylindrical filter compartment 120R and a second waveguide filter F1L is implemented to the left in the filter compartment 120R. The filter compartment 120R is ro- tatable R a predetermined angle, here 180 degrees, around a rotation axis AV relative to a frame 325 so as to either engage the first waveguide filter F1H or the second waveguide filter F1L in one of the first or second waveguide conduits, say 121. Figu- re 3 shows a positioning of the filter structure 300 where the se- cond waveguide filter F1L is engaged in the first waveguide con- duit According to the invention, the analogous is true for the second waveguide conduit 122. This means that a separate filter struc- ture 300 may be devised for the second waveguide conduit 122, where a filter compartment 120R is rotatable 180 degrees around the rotation axis AV relative to the frame 325 so as toeither engage a first waveguide filter F2H or a second waveguide filter F2L in one of the second waveguide conduit Alternatively, the filter compartments 120T and 120R may be combined, i.e. be implemented parallel to one another, so that when such a combined filter compartment 120T/R is rotated 180 degrees a particular filter pair F1H and F1L or Fzn and Fzt is si- multaneously engaged in the first and second waveguide con- duits 121 and 122 respectively. For example, the first waveguide filter pair F1H, Fzn may be adapted for radio communication at a higher band than the second waveguide filter pair F1L, Fzt. Fi- gure 9 shows one example of such an implementation. ln the embodiment shown in Figure 3, the rotation axis AV is perpendicular to a flat surface 330 onto which the frame 325 is mounted via attachments means, e.g. screws, schematically il- lustrated as 311, 312, 313 and 314 in Figure According to embodiments of the invention, the filter compart- ment 120T/R may be configured to be manually rotated R by a user of the terminal 100, be rotated by means of an electric mo- tor (not shown), or both. Naturally, the electric motor may alter- natively be represented by any other type of automatically con- trollable actuator device, e.g. a microelectromechanical actu- ator, such as a comb drive, a hydraulic piston, a relay, a thermal biomorph, a digital micromirror device, a piezoelectric actuator, an electroactive polymer or a servo mechanism.

According to one embodiment of the invention, the filter struc- ture 300 contains a sensor arrangement configured to produce a signal sL/H indicating which of the first and second waveguide filter pairs F1H, Fzn or Fit, Fzt respectively that is engaged in the first and second waveguide conduits 121 and 122. Figure 3 rep- resents such a sensor arrangement by a sensor 350 and first and second transponders 351 and 352 at the first and second waveguide filter pairs F1H, Fzn or Fit, Fzt respectively.Preferably, the sensor arrangement 350, 351 and 352 is further configured to indicate if the one of the first or the second wave- guide filter pairs F1H, Fzn or F1L, Fzt that is engaged in the first and second waveguide conduits 121 and 122 is properly posi- tioned therein.

Figure 4 illustrates a filter structure 400 according to a second embodiment of the invention. The filter structure 400 is carried in a frame being represented by two rings 425a and 425b res- pectively that are mounted on a flat surface 430 via schematic legs 411 and 412. ln contrast to Figure 3, here, a rotation axis AP around which the filter structure 400 is rotated a predetermi- ned angle to either engage the first waveguide filter pair F1H, F2H or the second waveguide filter pair Fit, Fzt in the first and se- cond waveguide conduits 121 and 122, is parallel to the flat sur- face 430 onto which the frame 425a and 425b is mounted. How- ever, analogous to the embodiment of Figure 3, the predeter- mined angle is 180 degrees. This means that the first or the se- cond waveguide filter pairs F1H, Fzn or Fn, Fzt are positioned back to back in the filter structure As mentioned above, the filter compartment 120T/R may be con- figured to be manually rotated R by a user of the terminal 100, be rotated by means of an electric motor, (or other type of auto- matically controllable actuator device) or a combination thereof. Figure 4 exemplifies a motor 410 having a shaft 415 with a gear 417. A belt 422 embraces the gear 417 and a drive ring 425 of the filter compartment 120T/R. Consequently, in response to a control signal C received in the electric motor 410, the electric motor 410 may cause the filter compartment 120T/R to rotate R the predetermined angle.

Figures 5a and 5b illustrate a filter structure 500 according to a third embodiment of the invention. As in Figure 3, the filter structure 500 carries the filter compartment 120T/R in frame 525 that is mounted onto a flat surface 530, for example via attach- ment means 511, 512, 513 and 514, e.g. in the form of screws.Similar to the embodiment of Figure 3, the rotation axis AV is perpendicular to the flat surface Here, however, the predetermined angle at which the filter com- partment 120T/R is rotatable R around the rotation axis AV rela- tive to the frame 525 so as to either engage the first waveguide filter pair F1H, Fzn or the second waveguide filter pair F1L, Fzt in the first and second waveguide conduits 121 and 122 is 90 de- grees. Therefore, to attain a low overall profile of the filter struc- ture 500, the first waveguide filter pair F1H, F2H and the second waveguide filter pair F1L, Fzt are preferably interleaved on top of one another as illustrated in Figure 5b Figure 6 illustrates a filter structure 600 according to a fourth embodiment of the invention. Analogous to the second em- bodiment of Figure 4, the filter structure 600 is carried in a fra- me represented by two rings 625a and 625b respectively that are mounted on a flat surface 630 via schematic legs 611 and 612; and the rotation axis AP is parallel to the flat surface 630. ln contrast to Figure 4 and similar to Figures 5a and 5b, the pre- determined angle at which the filter compartment 120T/R is ro- tatable R around the rotation axis AP relative to the frame 625a and 625b so as to either engage the first waveguide filter pair F1H, Fzn or the second waveguide filter pair F1L, Fzt in the first and second waveguide conduits 121 and 122 is 90 degrees.

Figure 6 further shows an electric motor 610 (which equally well may be represented by another type of automatically control- lable actuator device) having a shaft 615 with a gear 617. A belt 622 embraces the gear 617 and a drive ring 625 of the filter compartment 120T/R. Consequently, in response to a control signal C received in the electric motor 610, the electric motor 610 may cause the filter compartment 120T/R to rotate R the predetermined angle. Alternatively, or additionally, the filter compartment 120T/R may rotated R manually by a user of the terminalFigures 4 to 6 exemplify embodiments of the invention, wherein the predetermined angle by which the filter compartment 120T/R is rotatable to either engage the first waveguide filter pair Fm, F2H or the second waveguide filter pair F1L, Fzt in the first and second waveguide conduits 121 and 122 is either 90 or 180 de- grees.

A predetermined rotation of 180 degrees is generally advanta- geous because it enables a slim design in relation to the flat surface, especially if the rotation axis is perpendicular to this surface. Namely, in such a case the first and second waveguide filters may be arranged side by side with a respective lowest si- de protruding from the flat surface.

A predetermined rotation of 90 degrees is generally advanta- geous because it requires less movement when switching bands. l\/lore important, however, a design involving 90 degrees rotation accomplishes a maximal distance between the engaged and non-engaged waveguide filters. This, in turn, vouches for small signal leakage via the non-engaged filter.

Although being generally less desirable than 90 and 180 de- grees, according to the invention, it is technically possible to se- lect any other predetermined angle that is large enough to ac- commodate the first and second waveguide filters in the filter compartment.

Figures 7 to 9 illustrate various leakage reduction components according to embodiments of the invention. lt should be noted that the geometry shown in Figure 7 represents volumes filled with air or other non-conducting material in the first and second waveguide conduits 121 and 122 respectively.

Figure 7 represents a first waveguide filter F1H/F2H and a second waveguide filter F1L/F2L in a filter compartment 120T/R that is rotatable as described above with reference to Figure 3. ln Figu- re 7, the filter compartment 120T/R has been positioned such that the second waveguide filter F1L/F2L, is engaged in a wave- guide conduit. As a result, electromagnetic energy may pass from an input 721 to an output 722 of the filter structure.

Leakage reduction components in the form of a first waveguide choke 735 and a second waveguide choke 736 are here configu- red to screen off electromagnetic energy from the input 721 and the output 722 respectively.

Figure 7 represents an air slot 730 between filter compartment 12OT/R and the frame 325. To reduce signal leakage along the air slot 730, the air slot 730 should be narrow, say in the order of 50 um (for the Ku band). lt is further preferable if one or more stub elements are arranged in the outer wall of the filter com- partment 12OT/R. Figure 7 shows four such stub elements in the form of openings 731, 732, 733 and 734. Each of these stub ele- ments is configured to prevent leaking electromagnetic energy from propagating along the outer wall of the filter compartment 12OT/R.

Figure 8 shows a filter compartment 12OT/R that is rotatable as described above with reference to Figure 3. Rotation of the filter compartment 12OT/R in the frame 325 is facilitated by means of first and second bearing rings 821 and 822 disposed around the filter compartment 12OT/R. ln Figure 8 leakage reduction com- ponents are represented by a number of spring-assisted contact members, say 2-4, here represented by 831, 832 and 833 arran- ged in the first and/or the second bearing ring 822. Each of the contact members is configured to cause galvanic contact bet- ween the filter compartment 12OT/R and the frame 325 thus shortcutting any leaking electromagnetic energy.

Figure 9 illustrates a filter structure according to one embodi- ment of the invention, where the filter compartments 12OT and 12OR for transmission and reception respectively are combined and implemented parallel to one another in a single frame 325. Thus, when the combined filter compartment 12OT/R is rotated 180 degrees, either a first filter pair Fit and Fzt is simultane-ously engaged in the first and second waveguide conduits 121 and 122 respectively, or a second filter pair F1H and Fzn is simul- taneously engaged in the first and second waveguide conduits 121 and 122 respectively.

More precisely, in a first positioning of the combined filter com- partment 12OT/R, the first filter pair F1L and Fzt is set such that a first low-band filter component F1L is coupled between a trans- mitter input 721T and a transmitter output 722T in the frame 325 and a second low-band filter component F2L is coupled between a receiver input 721R and a receiver output 722R in the frame 325 (as illustrated in Figure 9). Analogously, in a second posi- tioning of the combined filter compartment 12OT/R, the second filter pair F1H and F2H is set such that a first high-band filter component Fin is coupled between the transmitter input 721T and the transmitter output 722T and a second high-band filter component F2H is coupled between the receiver input 721R and the receiver output 722R.

Figures 10a and 11a show frequency graphs illustrating a first combination of a receiver-transmitter pair of filters according to one embodiment of the invention. The graphs represent a sym- bolic signal gain |S12| in a linear scale from O to 1 along the vertical axes and frequency along the horizontal axes. As dis- cussed above with reference to Figures 2a and 2b, the pass- bands PBH1 and PBL1 and stop bands are such that they may be used interchangeably for transmission and reception without risk of interference.

Figures 10b and 11b show frequency graphs illustrating a se- cond combination of a receiver-transmitter pair of filters accor- ding to one embodiment of the invention. Also here, the graphs represent a symbolic signal gain |S12| in a linear scale from O to 1 along the vertical axes and frequency along the horizontal axes; and the passbands PBH2 and PBL2 and stop bands are such that they may be used interchangeably for transmission and reception without risk of interference.Variations to the disclosed embodiments can be understood and effected by those skilled in the art in practicing the claimed in- vention, from a study of the drawings, the disclosure, and the appended claims.

The term "comprises/comprising" when used in this specification is taken to specify the presence of stated features, integers, steps or components. The term does not preclude the presence or addition of one or more additional elements, features, inte- gers, steps or components or groups thereof. The indefinite ar- ticle "a" or "an" does not exclude a plurality. ln the claims, the 10 word "or" is not to be interpreted as an exclusive or (some- times referred to as "XOR"). On the contrary, expressions such as "A or B" covers all the cases "A and not B", "B and not A" and "A and B", unless otherwise indicated. The mere fact that certain measures are recited in mutually different dependent claims does not indicate that a combination of these measures cannot be used to advantage. Any reference signs in the claims should not be construed as limiting the scope. lt is also to be noted that features from the various embodiments described herein may freely be combined, unless it is explicitly stated that such a combination would be unsuitable.

The invention is not restricted to the described embodiments in the figures, but may be varied freely within the scope of the claims.

Claims

1. A terminal (100) for dual-band radio communication with spacecrafts, the terminal (100) comprising: an antenna unit (110) configured to exchange radio-fre- quency signals (RFR; RFT) bidirectionally with the spacecrafts, a first amplifying and frequency-mixing circuitry (130) con- figured to up convert an outgoing modulated signal (TX) to be fed through a first waveguide conduit (121) connected to the an- tenna unit (110), a second amplifying and frequency-mixing circuitry (150) configured to down convert an incoming signal (Rvv) received through a second waveguide conduit (122) connected to the an- tenna unit (110), and a modulator-demodulator unit (140) configured to trans- form an outgoing baseband signal (BBT) into the outgoing modu- lated signal (TX) and transform the incoming signal (Rw) into a received baseband signal (BBR), wherein each of the first and second waveguide conduits (121; 122) is arranged to forward radio-frequency signals on at least two separate bands (F1H, Fn; Fzn, Fzt), characterized in that the first and second waveguide conduits (121; 122) comprise a respective or a common filter compart- ment (120T/R) being rotatable (R) a predetermined angle around a rotation axis (AV, AP) relative to a frame (325; 425a, 425b; 525; 625a, 625b) comprised in a filter structure (300, 400, 500, 600) comprisinq the frame carryinq a filter compartment that holds first and second waveguide filter pairs (Fm, F2H; Fn, FZL), and the filter structure is configured se-as to either selectively engage either the a first waveguide filter pair (F1H, Fzn) or a th_e second waveguide filter pair (Fn, Fzt) in the first and second waveguide conduits (121; 122), which first waveguide filter pair (Fm, Fzn) is adapted for radio communication at a higher band than the second waveguide filter pair (Fn, Fzt).

2. The terminal (100) according to claim 1, wherein said filter compartment (120T/R) is rotatable (R) 180 degrees around the rotation axis (AV, AP) relative to the frame (325; 425a, 425b).

3. The terminal (100) according to claim 1, wherein said filter compartment (120T/R) is rotatable (R) 90 degrees around the rotation axis (AV, AP) relative to the frame (525; 625a, 625b).

4. The terminal (100) according to any one of the preceding claims, wherein the rotation axis (AV) is perpendicular to a flat surface (330, 530) onto which the frame (325, 525) is mounted.

5. The terminal (100) according to any one of the claims 1 to 3, wherein the rotation axis (AP) is parallel to a flat surface (430, 630) onto which the frame (425a, 425b; 625a, 625b) is mounted.

6. The terminal (100) according to any one of the preceding claims, wherein said filter compartment (120T/R) is configured 10 to be manually rotated (R) by a user of the terminal (100).

7. The terminal (100) according to any one of the preceding claims, comprising an automatically controllable actuator device (410, 610) configured to cause said filter compartment (120T/R) to rotate (R) in response to a control signal (C).

8. The terminal (100) according to any one of the preceding claims, comprising a sensor arrangement (350, 351, 352) confi- gured to produce a signal (st/H) indicating which of the first and second waveguide filter pairs(F1H, FzH; Fn, Fzt) that is engaged in the first and second waveguide conduits (121; 122).

9. The terminal (100) according to claim 8, wherein the sen- sor arrangement (350, 351, 352) is further configured to indicate if the one of the first or the second waveguide filter pairs (Fin, FzH; F1L, Fzt) being engaged in the first and second waveguide conduits (121; 122) is properly positioned therein.

10. A filter structure (300, 400, 500, 600) for engaging selecti- vely either a first waveguide filter giir (F1H; Fzn) or a second wave-guide filter pa_ir (F1L; Fzt) in a waveguide conduit (121; 122) thus rendering the waveguide conduit (121; 122) adapted for forwarding radio-frequency signals at a higher band (PBH1; PBH2) or a lower band (PBL1; PBL2) respectively, characterized in that the filter structure comprises a frame (325; 425a, 425b; 525; 625a, 625b) carrying a filter compart- ment (120T, 120R) that holds the first and second waveguide filters i (Fin, F2H; F1L, Fzt), and the filter compartment (120T, 120R) is rotatable (R) a predetermined angle around a rotation axis (AV, AP) relative to the frame (325; 425a, 425b; 525; 625a, 625b) so as to either engage the first waveguide filter pa_ir(F1H, Fzn) or the second waveguide filter giir (Fn, Fzt) in the waveguide conduit (121; 122).

11. The filter structure (300, 400, 500, 600) according to claim 10, comprising at least one leakage reduction component (731, 732, 733, 734, 735, 736, 831, 832, 833) configured to reduce an outflow of signal energy outside of the first or second waveguide filter pa_ir (Fm, FzH; F1L, Fzt) respectively being engaged in the waveguide conduit (121; 122).

12. The filter structure (300, 400, 500, 600) according to claim 11, wherein the at least one leakage reduction component com- prises at least one of: at least one waveguide choke (735, 736) configured to screen off electromagnetic energy from an input (721) to or an output (722) from the filter structure; at least one stub element (731, 732, 733, 734) arranged in an outer wall of the filter compartment (120T, 120R), which at least one stub element is configured to prevent leaking electro- magnetic energy from propagating along said outer wall; andat least one spring-assisted contact member (831, 832, 833) arranged in a bearing ring (822) of the filter compartment (12OT, 12OR), which at least one contact member is configured to cause galvanic contact between the filter compartment (12OT, 12OR) and the frame (325) thus shortcutting any leaking electro- magnetic energy.