U.S. patent number 3,665,481 [Application Number 05/036,531] was granted by the patent office on 1972-05-23 for multi-purpose antenna employing dish reflector with plural coaxial horn feeds.
Invention is credited to George M. Low, N/A, Kenneth E. Woo.
United States Patent |
3,665,481 |
Low , et al. |
May 23, 1972 |
MULTI-PURPOSE ANTENNA EMPLOYING DISH REFLECTOR WITH PLURAL COAXIAL
HORN FEEDS
Abstract
A microwave antenna useful on a spacecraft, which utilizes a
single dish reflector and single coaxial horn structure to transmit
at two frequencies, and to receive signals at a third frequency
that allow tracking. The horn structure includes a coaxial
wave-guide with an inner pipe for transmitting X-band waves, an
intermediate pipe, surrounding the inner pipe for transmitting
S-band waves through the space between it and the inner pipe, and
an outer pipe surrounding the intermediate pipe for receiving
S-band tracking signals. An outer horn flares from the outer pipe
and an inner horn flares from the inner pipe, to efficiently
illuminate the dish reflector at both X and S bands.
Inventors: |
Low; George M. (N/A),
N/A (South Pasadena, CA), Woo; Kenneth E. |
Family
ID: |
21889104 |
Appl.
No.: |
05/036,531 |
Filed: |
May 12, 1970 |
Current U.S.
Class: |
343/762; 342/365;
342/432; 343/779; 343/853; 342/425; 343/777; 343/786 |
Current CPC
Class: |
H01P
1/16 (20130101); H01Q 25/04 (20130101) |
Current International
Class: |
H01Q
25/00 (20060101); H01Q 25/04 (20060101); H01P
1/16 (20060101); H01q 019/14 () |
Field of
Search: |
;343/776,777,778,779,786,762,853 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Lieberman; Eli
Claims
What is claimed is:
1. Apparatus for indicating the pointing error of an antenna from a
source of circularly polarized waves comprising:
a signal detecting structure including a circular coaxial waveguide
with inner and outer coaxial pipes, and a plurality of conductive
plates extending radially between said pipes;
a plurality of probes spaced about said waveguide for detecting
transverse electric and magnetic waves therein;
first means coupled to said probes for deriving the TE.sub.11
component and deriving the TM.sub.01 component in said waveguide;
and
second means coupled to said first means for generating signals
indicating the relative magnitudes and relative phases of said
TE.sub.11 and TM.sub.01 components.
2. The apparatus described in claim 1 including:
antenna orienting means responsive to the presence of a
predetermined ratio of the TM.sub.01 component to the TE.sub.11
component, for rotating said signal detecting structure in a
direction dependent upon the phase difference between the TM.sub.01
and TE.sub.11 components.
3. Apparatus for indicating the pointing error of an antenna from a
source of circularly polarized waves comprising:
a circular coaxial waveguide with inner, intermediate, and outer
coaxial pipes;
a first circular horn extending from said outer pipe of said
waveguide;
a second horn smaller than said first horn extending from said
inner pipe;
a reflector of larger diameter than said first horn positioned
opposite said first horn, said second horn extending from said
inner pipe towards said reflector;
a plurality of probes spaced about said waveguide for detecting
transverse electric and magnetic waves therein;
first means coupled to said probes for deriving TE.sub.11 and
TM.sub.01 components in said waveguide; and
second means coupled to said first means for generating signals
indicating the relative magnitudes and relative phases of said
TE.sub.11 and TM.sub.01 components.
4. An antenna comprising:
a reflector dish;
a coaxial waveguide extending toward said dish, said waveguide
having inner, intermediate, and outer guides, said inner guide less
than about one-half the diameter of said outer guide;
a first horn flaring out from said outer guide toward said
dish;
a second horn flaring out from said inner guide toward said dish;
and
a plurality of probes disposed about the annular space between said
outer and intermediate guides, for enabling the detection of the
TE.sub.11 and TM.sub.01 modes therein.
5. A microwave antenna structure comprising:
a coaxial waveguide having inner, intermediate, and outer coaxial
pipes, and having a radiating end;
first means for generating microwaves of a first frequency coupled
to said outer pipe;
second means for generating microwaves of a second frequency higher
than said first frequency coupled to said inner pipe;
a common dish reflector located opposite said radiating end of said
coaxial waveguide; and
a plurality of conductive plates extending radially between two of
said pipes and parallel to the axis of said coaxial waveguide, for
dividing the coaxial area between the two pipes into a plurality of
quasi-rectangular waveguides.
6. A microwave structure comprising:
an antenna structure including a coaxial waveguide having inner and
outer coaxial pipes, and a circular horn flaring outwardly from an
end of said outer pipe;
four conductive plates extending radially between the inner and
outer pipes and parallel to the axis of said coaxial waveguide, for
dividing the coaxial area into four quasi-rectangular waveguides
that each subtend an angle of approximately 90.degree. about the
axis of said waveguide;
four probe means, each disposed in said quasi-rectangular
waveguides for detecting microwaves therein; and
means coupled to said probe means for deriving first and second
signals respectively representing the relative amplitude and
relative phase of TE.sub.11 and TM.sub.01 waves in the coaxial
region between said pipes.
7. The structure described in claim 6 including:
antenna orienting means responsive to said first and second
signals, for reorienting said antenna structure upon the detection
of a predetermined ratio of said TM.sub.01 and TE.sub.11 waves, in
directions dependent upon the phase difference between said
TE.sub.11 and TM.sub.01 waves.
Description
ORIGIN OF THE INVENTION
The invention described herein was made in the performance of work
under a NASA contract and is subject to the provisions of Section
305 of the National Aeronautics and Space Act of 1958, Public Law
85-568, (72 Stat. 435; 42 USC 2457).
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates to antenna systems.
2. Description of the Prior Art
One type of spacecraft designed for deep space missions requires
antennas for transmitting at S-band and X-band frequencies, and for
receiving command signals and determining their direction of origin
so that the craft can orient its antennas precisely towards the
earth tracking station. This generally would necessitate three
separate antenna structures, with three horns and possibly three
reflectors. If such antenna capabilities could be combined in a
single antenna structure, space and weight could be saved on the
craft.
OBJECTS AND SUMMARY OF THE INVENTION
An object of the present invention is to provide a compact antenna
structure having many antenna capabilities.
Another object is to provide a simple and highly efficient
apparatus for tracking a microwave source.
In accordance with one embodiment of the invention, a microwave
antenna structure is provided which combines tracking and
transmission at two different frequencies in a single waveguide and
horn assembly that can be utilized with a single reflector. The
apparatus includes three coaxial pipes, the innermost pipe carrying
X-band waves for transmission, the space between the intermediate
and innermost pipe carrying S-band microwaves for transmission, and
the space between the outermost and intermediate pipe carrying
received S-band signals. One end of the pipes has a conical horn
spreading out from the outermost pipe and directed towards a
reflector to increase gain. In order to efficiently illuminate the
reflector with X-band microwaves from the innermost pipe, a small
additional horn is provided which flares from the innermost pipe
towards the reflector.
The region between the intermediate and outermost pipes is utilized
for tracking to determine the angle between the received beams
which were transmitted by the earth station and the direction in
which the antenna points, so that the antenna can be pointed
precisely at the earth station. This is accomplished by employing
four conductive plates which divide this outer waveguide region
into four quasi-rectangular waveguides. When a circularly polarized
wave transmitted by the earth station is received at this outer
region, both TE.sub.11 and TM.sub.01 waves are generally propagated
in the region. Four probes are positioned in the four
quasi-rectangular waveguides to pick up these waves. The four
probes are connected to a hybrid circuit which has two outputs, one
being the TE.sub.11 component and the other TM.sub.01 component.
The ratio of the amplitudes of these components indicates the error
angle between the antenna pointing direction and the source of the
signals (the direction of the earth station), while the phase
between these two signals indicates the direction in which the
antenna must be rotated to reduce the error angle. Signals
representing these amplitude and phase relationships can be used to
reorient the antenna.
The novel features of the invention are set forth with
particularity in the appended claims. The invention will be best
understood from the following description when read in conjunction
with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a partial perspective, partial schematic diagram of
antenna apparatus constructed in accordance with the present
invention;
FIG. 2 is a partial schematic diagram of the antenna apparatus,
showing the circuit for tracking an incoming signal;
FIG. 3 is a partial perspective view of an antenna horn;
FIG. 4 is a graph showing the relationship between the amplitudes
of the TE.sub.11 and TM.sub.01 components and the pointing cone
error angle of the antenna; and
FIG. 5 is a graph showing the relationship between the phase
difference of the TM.sub.01 and TE.sub.11 components and the
angular direction of the pointing error.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
As shown in FIG. 1, an antenna structure is provided for
transmitting and receiving signals, including a waveguide assembly
10, a horn assembly 12 at one end of the waveguide assembly which
serves largely as a radiating end, and a reflector 14 positioned
opposite the horn assembly. The waveguide assembly 10 includes a
circular inner tube 16 for carrying an X-band signal at a frequency
such as 8,448 MHz, an intermediate tube 18 more than twice the
diameter of the inner tube for carrying an S-band signal in the
region between it and the small inner tube, of a frequency such as
2,295 MHz, and an outer tube 20 for carrying a received S-band
signal of a frequency such as 2,115 MHz. An X-band source 22
generates X-band signals which pass through the inner tube for
transmission of information while an S-band source 24 is coupled to
the intermediate tube 18 to transmit information at S-band. The
reason why both frequency bands are utilized in transmission is
that while X-band allows more information to be transmitted and is
more efficient, these waves cannot always penetrate earth's
atmosphere. On the other hand, S-band signals generally can
penetrate the earth's atmosphere even under adverse conditions, for
receipt by an earth ground station.
The signal received in the tracking region 21 between the outer
tube 20 and intermediate tube 18 enables tracking, so that the
antenna can be pointed precisely toward the earth station which
transmitted the signal. If the earth station transmits a circularly
polarized signal of proper frequency, the received signal will
produce TE.sub.11 components and TM.sub.01 components in the
tracking region 21 between the outer pipe 20 and the intermediate
pipe 18. In the absence of a circular horn, the TE.sub.11 and
TM.sub.01 components will not be produced, and instead only
TE.sub.10 waves will be produced in the tracking region 21 (then
the structure would act as a four horn monopulse tracking system
and three channels would have to be generated initially and dealt
with). The relative strength of these components (TE.sub.11 and
TM.sub.01) and their relative phase can be utilized to determine t
the error cone angle between the earth station and the direction in
which the antenna is pointing, as well as the direction in which
the antenna must be moved for better alignment.
In order to detect the TE.sub.11 and TM.sub.01 components, four
probes 26, 28, 30 and 32 are provided which project into the
tracking region 21. The signals picked up by the four probes are
fed to a detecting circuit 34 with one output 36 that delivers the
TE.sub.11 components and another output 38 which delivers the
TM.sub.01 component. These two outputs are connected to antenna
orienting apparatus 40 which can rotate the antenna to point it
more precisely towards the earth station which transmitted the
tracking signal. The orienting apparatus 40 includes an amplitude
comparor circuit 41 for determining the ratio of the two components
to determine the cone angle of error as well as a phase comparor
circuit 43 for determining the relative phase of two components to
determine the direction in which the antenna must be reoriented to
reduce the pointing error. The antenna orienting apparatus also
includes a drive 45 which may operate gas jets or the like to
reorient the antenna, or even the entire spacecraft in those cases
where the antenna is rigidly fixed to the craft.
The two S-band signals which are carried by the antenna, one for
transmitting and one for receiving, are close enough in frequency
so that a single horn 42 can be employed to efficiently illuminate
the reflector 14 with both frequencies. However, the X-band signal
passing through the inner tube 16 has a frequency more than twice
as great as either S-band frequency, and its beam width is too
narrow to efficiently illuminate the reflector. In order to
increase the beamwidth at X-band, an additional horn 44 is
utilized, which flares from the outer end of tube 16. The horn 44
blocks a small portion of the radiating aperture for the S-band
signal, but it greatly increases the efficiency of radiation of the
X-band signal when the same reflector 14 is used for both frequency
bands. It would be possible to obtain a greater beamwidth without
the use of the second horn 44, by exciting various higher modes in
the inner tube 16, through the use of discontinuities and the like.
However, this would increase the complexity and weight of the
antenna structure. The use of only the small additional horn 44
provides good overall efficiency in a simple and light structure.
It may be noted that, although a reflector 14 is generally employed
to increase gain, it is possible to dispense with this and radiate
directly from the horns (but then a four horn monopulse tracking
technique would have to be used for any tracking). Also, although
the horn is shown located in front of the reflector, various
telescope constructions can be used such as Cassegrain types
wherein the horn energy is radiated by a subreflector towards the
main reflector dish.
As shown in FIG. 2, the tracking region 21 is divided by four
electrically conductive plates 46, into four quasi-rectangular
waveguides 48, 50, 52 and 54. Each of the probes 26, 28, 30 and 32
is positioned at the center of one of these quasi-rectangular
wave-guides to detect the microwave signal therein. The TE.sub.11
and TM.sub.01 modes propagating through the tracking region can be
separated by a hybrid circuit of the type shown in FIG. 2 which
includes two hybrid rings or magic tees 56, 58, and two 3 db
hybrids 60 and 62. The probes 28 and 32 are connected to two ports
of one ring 56 while the other probes 26, 30 are connected to two
ports of another ring 58. The difference signal port .DELTA. from
each ring 56, 58 is connected to 90.degree., 3 db hybrid 60 which
delivers only the TE.sub.11 mode on line 64. The sum signal port
.epsilon. from each ring 56, 58 is connected to 0.degree., 3 db
hybrid 62 which delivers the TM.sub.01 component on a line 66.
Thus, the hybrid circuit delivers signals representing these two
modes separately. In a laboratory set-up, these two signal
components can be delivered to a comparor 68 that shows their
relative amplitudes and phases. A switch 69 can be moved between
either of two positions to indicate relative amplitude or phase on
a meter 71. Knowledge about the relative amplitudes and phases can
be used to determine the angular deviation or error of the antenna
line of sight or boresight from the earth station, as well as the
direction of that error.
FIG. 3 illustrates the horn 12 and a system of coordinates for
indicating the cone angle .theta. and position angle .phi. which
define the direction of an incoming signal S with respect to the
line of sight L of the antenna. FIG. 4 illustrates the relationship
between the amplitudes of the TE.sub.11 and TM.sub.01 modes as a
function of the cone angle .theta.. It can be seen that the
TM.sub.01 mode decreases rapidly towards a null as the cone angle
.theta. decreases towards zero, that is, as the antenna becomes
precisely aligned with the direction of the tracking signal. By
calculating the ratio of the TE.sub.11 and TM.sub.01 components, or
measuring the amplitude of the TM.sub.01 mode under conditions
where the incoming signal is relatively constant, one can determine
the approximate cone angle. FIG. 5 illustrates the relative phases
of the TM.sub.01 and TE.sub.11 modes as the position angle .phi.
varies. It can be seen that the phase difference of the components
is proportional to the position angle .phi., and a comparison of
the phases indicates the position angle at which the incoming
signal is being received when the antenna is not aligned with the
direction of the incoming tracking signal. Circuitry is well known
which can be utilized to automatically calculate the ratio of
magnitudes and relative phases of the two components to drive a
reorienting system that reorients the antenna to point directly
towards the source of the tracking signals.
An antenna structure of the type shown in FIG. 2 has been
constructed, using a Hewlett Packard Model HP8410 network analyzer
as the amplitude and phase comparor 68. Microwaves were directed at
the structure at various positions relative to the pointing
direction of the structure, and graphs were made of the types shown
in FIGS. 4 and 5 (where only an outer horn 12 but no inner horn 44
was present). FIG. 4 represents the signal levels for the two
components which were obtained while FIG. 5 represents the phase
relationships which were obtained at the various position angles.
It may be noted that in an ideal case, the graph of FIG. 5 would be
a straight line, and in FIG. 4 the TM.sub.01 mode would achieve a
null at a zero degree cone angle.
Thus the invention provides a compact antenna structure having
multiple capabilities, including the ability to transmit at two
widely different frequencies and to receive at still another
frequency. The invention also provides an improved tracking system
for detecting the direction of a tracking signal.
Although particular embodiments of the invention have been
described and illustrated herein, it is recognized that
modifications and variations may readily occur to those skilled in
the art and, consequently, it is intended that the claims be
interpreted to cover such modifications and equivalents.
* * * * *