JP2009074902A - Satellite-mounted antenna pattern measurement method - Google Patents
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本発明は、人工衛星搭載アンテナにおけるアンテナパタン測定方法に関するものである。より詳細には、複数の地球局設備を使用することで、衛星姿勢制御回数を大幅に削減すると共に、姿勢制御誤差に伴う角度誤差の校正および地球局設備の校正を実現し、精度の高いアンテナパタン測定を実現する方法に関する。 The present invention relates to an antenna pattern measuring method for an antenna mounted on a satellite. More specifically, by using multiple earth station equipment, the number of satellite attitude control operations can be greatly reduced, and angle error calibration and earth station equipment calibration associated with attitude control errors can be achieved, thereby providing a highly accurate antenna. The present invention relates to a method for realizing pattern measurement.
従来の技術1における衛星搭載アンテナのアンテナパタン測定方法は、非特許文献1に記載されているとおり、衛星からの一定の電力を送信した状態で、搭載アンテナの出力信号を単一の地球局設備にて受信電力レベルを測定し、仰角オフセット量の異なる方位角カットパタンを生成し、図1に示すようにロール軸の設定角度を一定の増減分で順次変え、複数の方位角カットパタンを取得することを繰り返し、2次元アンテナパタンを測定している。この場合、衛星の姿勢制御回数が非常に多くなると共に、測定時間を要する。さらに、後述する従来の技術2と同様、衛星姿勢制御誤差の影響も挙げられる。 As described in Non-Patent Document 1, the method for measuring the antenna pattern of a satellite-mounted antenna according to the conventional technique 1 uses a single earth station equipment to output an output signal of the mounted antenna in a state in which a constant power from the satellite is transmitted. Measure the received power level at, generate azimuth cut patterns with different elevation offsets, and sequentially change the roll axis setting angle by a certain increment or decrement as shown in Fig. 1 to obtain multiple azimuth cut patterns The two-dimensional antenna pattern is measured repeatedly. In this case, the number of times of attitude control of the satellite is extremely increased, and measurement time is required. Furthermore, the influence of the satellite attitude control error can be mentioned as in the conventional technique 2 described later.
一方、従来の技術2における衛星搭載アンテナのアンテナパタン測定方法は、非特許文献2に記載されているように、図2に示すように複数の地球局設備を用い、より少ない衛星の姿勢制御回数で2次元アンテナパタンを測定する方法が述べられている。しかしながら、誤差要因として地球局設備の特性ばらつき、衛星姿勢制御誤差が挙げられる。 On the other hand, as described in Non-Patent Document 2, the conventional antenna pattern measurement method for satellite-mounted antennas uses a plurality of earth station facilities as shown in FIG. Describes a method for measuring a two-dimensional antenna pattern. However, error factors include variations in characteristics of earth station equipment and satellite attitude control errors.
従来の技術1の課題は、衛星姿勢制御の回数が非常に多くなり、多大な測定時間を要することである。従来の技術2の課題は、従来の技術1の衛星姿勢制御の回数および測定時間の課題が解決されているが、複数の地球局設備の特性ばらつきや、衛星姿勢制御誤差による測定誤差が挙げられる。 The problem of the prior art 1 is that the number of times of satellite attitude control becomes very large and a long measurement time is required. The problem of the conventional technique 2 is that the problems of the number of times of satellite attitude control and the measurement time of the conventional technique 1 are solved, but there are variations in characteristics of a plurality of earth station facilities and measurement errors due to satellite attitude control errors. .
本発明は従来の技術1および2の課題を解決し、衛星姿勢制御回数の削減、姿勢制御誤差に伴う角度誤差の補償、地球局設備の特性差の校正を実現して、精度の高い衛星搭載アンテナパタンの測定方法を提供することを目的とする。 The present invention solves the problems of the prior arts 1 and 2, reduces the number of satellite attitude control times, compensates for angle errors associated with attitude control errors, and calibrates the difference in characteristics of earth station equipment, so that it can be mounted on a highly accurate satellite. An object is to provide a method for measuring an antenna pattern.
上記目的を実現するため本発明による方法は、複数の地球局設備を用いて衛星搭載アンテナの2次元アンテナパタンを測定する方法において、人工衛星から一定電力の信号を該衛星搭載アンテナより出力し、該衛星搭載アンテナのロール軸周りの角度を一定値に設定し、ピッチ軸周りの角度を走査し、該衛星搭載アンテナの出力信号を該地球局設備にて受信電力レベルを測定し、該人工衛星のロール軸の設定角度および地球局設備の設置位置から、該人工衛星からの仰角オフセット量の異なる方位角カットパタンを該地球局設備と同数個生成する第1の生成ステップと、該人工衛星のロール軸の設定角度を一定の増減分で順次変え、前記第1の生成ステップを繰り返すことにより、複数の方位角カットパタンを生成する第2の生成ステップとを有し、前記一定の増減分と、該複数の地球局設備の何れか2つの該人工衛星からの仰角差が等しい角度である。 In order to achieve the above object, the method according to the present invention is a method of measuring a two-dimensional antenna pattern of a satellite-mounted antenna using a plurality of earth station facilities, and outputting a signal of constant power from an artificial satellite from the satellite-mounted antenna, The angle around the roll axis of the satellite-mounted antenna is set to a constant value, the angle around the pitch axis is scanned, the output signal of the satellite-mounted antenna is measured at the earth station facility, and the artificial satellite A first generation step of generating the same number of azimuth cut patterns with different elevation offsets from the satellite from the set angle of the roll axis of the earth station and the installation position of the earth station, A second generation step of generating a plurality of azimuth cut patterns by sequentially changing the set angle of the roll axis by a constant increase / decrease and repeating the first generation step; A, wherein a constant increment or decrement, the angular elevation difference is equal from any two of said satellites of said plurality of earth stations equipment.
このとき得られるカットパタンを図3に示す。ロール軸の設定角度の増減分と地球局設備の何れか2つの人工衛星からの仰角差が同一であるため、一部のカットパタンが重複する点が特徴である。このとき衛星姿勢誤差に伴う角度誤差が生じる場合、図4に示すように従来の技術2では角度誤差の検出ができないが、本発明においては、同一仰角のカットパタンが一致するように角度補正を行えばよいため、相対的な角度誤差を補償することができる。また、これら2つのカットパタンの受信レベルの差は、地球局設備の特性差であり、これについても補償することが可能となる。 The cut pattern obtained at this time is shown in FIG. Since the increase / decrease of the set angle of the roll axis and the elevation angle difference from any two artificial satellites of the earth station facility are the same, some cut patterns overlap. At this time, when an angle error due to the satellite attitude error occurs, the conventional technique 2 cannot detect the angle error as shown in FIG. 4, but in the present invention, the angle correction is performed so that the cut patterns of the same elevation angle coincide. Therefore, the relative angular error can be compensated. Further, the difference between the reception levels of these two cut patterns is a difference in characteristics of the earth station equipment, and this can also be compensated.
しかしながら、本手法では取得した全てのカットパタンに対して相対的な方位角誤差を補償することが可能であるが、地球局設備の特性差については、該人工衛星からの仰角差が同一である2局についてのみの補償に限定される。 However, this method can compensate for the relative azimuth angle error for all the acquired cut patterns, but the difference in elevation angle from the artificial satellite is the same as the characteristic difference of the earth station equipment. Limited to compensation for only two stations.
そこで、前述の衛星搭載アンテナパタン測定方法に、該衛星搭載アンテナのピッチ軸周りの角度を一定値に設定し、ロール軸周りの角度を走査し、該衛星搭載アンテナの出力信号を該地球局設備にて受信電力レベルを測定し、該人工衛星のピッチ軸の設定角度および地球局設備の設置位置から、該人工衛星からの方位角オフセット量の異なる仰角カットパタンを該地球局設備と同数個生成する第3の生成ステップをさらに加えることにより、地球局設備の校正を実施することが可能となる。このときに得られるカットパタンの一部を図5に示す。 Therefore, in the above-described satellite-mounted antenna pattern measurement method, the angle around the pitch axis of the satellite-mounted antenna is set to a constant value, the angle around the roll axis is scanned, and the output signal of the satellite-mounted antenna is output to the earth station equipment. Measure the received power level at, and generate the same number of elevation cut patterns with different azimuth offsets from the satellite from the set angle of the pitch axis of the satellite and the installation position of the earth station. By further adding the third generation step, it is possible to calibrate the earth station equipment. A part of the cut pattern obtained at this time is shown in FIG.
ここで、図中△で示した箇所は、図中中央部の地球局設備で取得される仰角カットパタンと図中右上部の地球局設備で取得される方位角カットパタンの交点であるため、本来は同一の値となる。しかしながら、地球局設備の特性に差が生じる場合、この差に応じて受信レベルに差が生じる。そこで、このレベル差を打ち消すようにすることで、2つの地球局設備の特性を校正することが可能となり、カットパタンの交点の一部および全てを利用することで、全ての地球局設備の校正が可能となる。 Here, the point indicated by Δ in the figure is the intersection of the elevation cut pattern acquired by the earth station equipment in the center of the figure and the azimuth cut pattern obtained by the earth station equipment in the upper right part of the figure, Originally the same value. However, when a difference occurs in the characteristics of the earth station equipment, a difference occurs in the reception level according to this difference. Therefore, by canceling out this level difference, it becomes possible to calibrate the characteristics of the two earth station facilities, and by using some and all of the intersections of the cut patterns, all the earth station facilities are calibrated. Is possible.
また、上記目的を実現するため本発明による方法は、複数の地球局設備を用いて衛星搭載アンテナの2次元アンテナパタンを測定する方法において、人工衛星から一定電力の信号を該衛星搭載アンテナより出力し、該衛星搭載アンテナのピッチ軸周りの角度を一定値に設定し、ロール軸周りの角度を走査し、該衛星搭載アンテナの出力信号を該地球局設備にて受信電力レベルを測定し、該人工衛星のピッチ軸の設定角度および地球局設備の設置位置から、該人工衛星からの方位角オフセット量の異なる仰角カットパタンを該地球局設備と同数個生成する第1の生成ステップと、該人工衛星のピッチ軸の設定角度を一定の増減分で順次変え、前記第1の生成ステップを繰り返すことにより、複数の仰角カットパタンを生成する第2の生成ステップと、有し、前記一定の増減分と、該複数の地球局設備の何れか2つの該人工衛星からの方位角差が等しい角度でもある。 In order to achieve the above object, the method according to the present invention is a method for measuring a two-dimensional antenna pattern of a satellite-mounted antenna using a plurality of earth station facilities, and outputting a signal of constant power from the satellite-mounted antenna. The angle around the pitch axis of the satellite-mounted antenna is set to a constant value, the angle around the roll axis is scanned, the output signal of the satellite-mounted antenna is measured at the earth station facility, and the received power level is measured. A first generation step of generating the same number of elevation cut patterns having different azimuth offset amounts from the artificial satellite from the setting angle of the pitch axis of the artificial satellite and the installation position of the earth station facility, and the artificial station A second generation step for generating a plurality of elevation cut patterns is performed by sequentially changing the set angle of the pitch axis of the satellite by a constant increase / decrease and repeating the first generation step. When has there the constant and increment or decrement, in angular orientation angle difference is equal to from any two of said satellites of said plurality of earth stations equipment.
この場合も、該衛星搭載アンテナのロール軸周りの角度を一定値に設定し、ピッチ軸周りの角度を走査し、該衛星搭載アンテナの出力信号を該地球局設備にて受信電力レベルを測定し、該人工衛星のロール軸の設定角度および地球局設備の設置位置から、該人工衛星からの仰角オフセット量の異なる方位角カットパタンを該地球局設備と同数個生成する第3の生成ステップをさらに加えることにより、地球局設備の校正を実施することが可能となる。 Also in this case, the angle around the roll axis of the satellite mounted antenna is set to a constant value, the angle around the pitch axis is scanned, and the output power level of the output signal of the satellite mounted antenna is measured by the earth station equipment. A third generation step of generating the same number of azimuth cut patterns having different elevation angle offset amounts from the artificial satellite from the set angle of the roll axis of the artificial satellite and the installation position of the earth station In addition, the earth station equipment can be calibrated.
また、前記第1の生成ステップの受信電力レベル測定は、該複数の地球局設備から一定電力の信号を該人工衛星に向けて送信し、該人工衛星の搭載アンテナによって受信した電力レベルの測定であることも好ましい。 The reception power level measurement in the first generation step is a measurement of a power level transmitted from the plurality of earth station facilities to the artificial satellite and received by the antenna mounted on the artificial satellite. It is also preferable that there is.
本発明の衛星搭載アンテナパタン測定方法は、複数の地球局設備を使用して、衛星姿勢制御の回数を大幅に削減すること共に、ロール軸(またはピッチ軸)の設定角度の増減分と地球局設備の何れか2つの該人工衛星からの仰角差(または方位角差)を同一とすることにより、衛星姿勢誤差の補償、地球局設備の特性偏差の校正を実現し、高精度のアンテナパタン測定を実現する。 The satellite-mounted antenna pattern measuring method of the present invention uses a plurality of earth station equipments to greatly reduce the number of satellite attitude controls, increase and decrease the set angle of the roll axis (or pitch axis), and the earth station. By making the elevation angle difference (or azimuth angle difference) from any two satellites of the equipment the same, it is possible to compensate for satellite attitude error and calibrate the characteristic deviation of the earth station equipment, and to measure the antenna pattern with high accuracy. Is realized.
本発明の第1の実施形態に係る衛星搭載アンテナパタン測定方法の概念図を図6に示す。静止軌道上における人工衛星aから一定電力の信号を搭載アンテナより出力した状態で、該人工衛星aのロール軸を所定の角度に設定し、ピッチ軸周りに角度走査するように制御を行い、該衛星搭載アンテナの出力信号を2以上の異なる地点に設置した地球局設備b1〜bnにて受信電力レベルを測定し、該人工衛星のロール軸の設定角度および地球局設備b1〜bnの設置位置から、該人工衛星からの仰角オフセット量の異なる方位角カットパタンc1−1〜cn−1を地球局設備b1〜bnと同数個生成し、ロール軸の設定角度を一定の増減分で順次変え、複数の方位角カットパタンc1−2〜cn−2,〜,c1−m〜cn−mを生成することを(m−1)回繰り返し、2次元アンテナパタンを測定する方法であって、ロール軸の設定角度の増減分と該地球局設備b1〜bnの何れか2つの該人工衛星aからの仰角差が同一である衛星搭載アンテナパタン測定方法である。 FIG. 6 shows a conceptual diagram of the satellite-borne antenna pattern measurement method according to the first embodiment of the present invention. In a state where a constant power signal is output from the onboard antenna from the satellite a on the geostationary orbit, the roll axis of the satellite a is set to a predetermined angle, and control is performed so as to scan the angle around the pitch axis The received power level is measured by the earth station equipment b1 to bn where the output signals of the satellite mounted antennas are installed at two or more different points. From the setting angle of the roll axis of the artificial satellite and the installation position of the earth station equipment b1 to bn The same number of azimuth cut patterns c1-1 to cn-1 with different elevation offsets from the satellite are generated as with the earth station facilities b1 to bn, and the set angle of the roll axis is sequentially changed by a certain increase / decrease, Is a method of measuring a two-dimensional antenna pattern by repeating (m-1) generations of azimuth cut patterns c1-2 to cn-2,..., C1-m to cn-m. Setting Elevation difference from any two of the satellites a of time the increment or decrement and the earth station equipment b1~bn is satellite antenna pattern measurement method is the same.
なお、図6の場合は、n=3(地球局設備は3つ)、m=3(方位角カットパタンの取得回数は3回)であり、地球局設備b1とb3の該人工衛星aからの仰角差が同一になっている。 In the case of FIG. 6, n = 3 (three earth station facilities), m = 3 (the azimuth cut pattern is acquired three times), and from the artificial satellite a of the earth station facilities b1 and b3. The elevation angle difference is the same.
このときカットパタンc3−1とc1−2、c3−2とc1−3は、同一の仰角オフセット量を有するため、衛星姿勢制御誤差が零であれば一致する。測定したカットパタンの一例を図7に示すが、衛星姿勢制御誤差および地球局設備b1,b3の特性差により両者は一致していないことが確認できる。ここでの角度誤差は方位角誤差に相当し、レベル差は地球局設備の特性差に相当しているため、図8に示すように方位角の相対誤差および受信レベル差を打ち消すようにオフセットさせることで、角度誤差とレベル差を補償することができる。 At this time, the cut patterns c3-1 and c1-2, and c3-2 and c1-3 have the same elevation angle offset amount, and therefore match if the satellite attitude control error is zero. An example of the measured cut pattern is shown in FIG. 7, and it can be confirmed that the two do not match due to the satellite attitude control error and the characteristic difference between the earth station facilities b1 and b3. The angle error here corresponds to the azimuth angle error, and the level difference corresponds to the characteristic difference of the earth station equipment. Therefore, as shown in FIG. Thus, the angle error and the level difference can be compensated.
本発明の第2の実施形態に係る衛星搭載アンテナパタン測定方法の概念図を図9に示す。第1の実施形態の衛星搭載アンテナパタン測定方法において、該人工衛星aのピッチ軸を所定の角度に設定し、ロール軸周りに角度走査するように制御を行い、該搭載アンテナの出力信号を2以上の異なる地点に設置した地球局設備b1〜bnにて受信電力レベルを測定し、該人工衛星aのピッチ軸の設定角度および地球局設備b1〜bnの設置位置から、衛星からの方位角オフセット量の異なる仰角カットパタンd1〜dnを地球局設備b1〜bnと同数個生成し、取得したカットパタンc1−1〜cn−1,〜,c1−m〜cn−m、d1〜dnの交点の受信レベルを比較することにより該地球局設備b1〜bnの受信特性を校正する衛星搭載アンテナパタン測定方法である。 FIG. 9 shows a conceptual diagram of the satellite mounted antenna pattern measuring method according to the second embodiment of the present invention. In the satellite-mounted antenna pattern measuring method of the first embodiment, the pitch axis of the artificial satellite a is set to a predetermined angle, and control is performed so as to scan the angle around the roll axis. The received power level is measured by the earth station facilities b1 to bn installed at the different points, and the azimuth offset from the satellite is determined from the set angle of the pitch axis of the artificial satellite a and the installation positions of the earth station facilities b1 to bn. The same number of elevation cut patterns d1 to dn as the earth station facilities b1 to bn are generated, and the obtained cut patterns c1-1 to cn-1, ..., c1-m to cn-m, d1 to dn This is a satellite-mounted antenna pattern measurement method for calibrating the reception characteristics of the earth station facilities b1 to bn by comparing reception levels.
図9の場合は、図6と同様にn=3(地球局設備は3つ)、m=3(方位角カットパタンの取得回数は3回)であり、地球局設備b1とb3の該人工衛星aからの仰角差が同一になっている。 In the case of FIG. 9, as in FIG. 6, n = 3 (three earth station facilities) and m = 3 (the number of azimuth cut pattern acquisition times is three), and the artificial of the earth station facilities b1 and b3 The elevation angle difference from the satellite a is the same.
第1の実施形態の測定方法においては、取得した全てのカットパタンc1−1〜cn−1,〜,c1−m〜cn−mに対して相対的な方位角誤差を補償することが可能であるが、地球局設備b1〜bnの特性差については、該人工衛星aからの仰角差が同一である2局についてのみの補償に限定される。そこで第2の実施形態の測定方法において、図9に示す△で示したカットパタンc3−1,c1−2,d2の交点において、受信レベルは同一になるため、地球局設備b1,b2,b3の特性を補償することが可能となる。測定した仰角カットパタンc1−2および方位角カットパタンd2を図10に示す。図中の△がそれぞれのc1−2およびd2の交点に対応する角度であり、これらの受信レベル差を打ち消すことで地球局設備b1,b2の特性を補償することが可能となる。 In the measurement method of the first embodiment, it is possible to compensate for the relative azimuth error with respect to all of the acquired cut patterns c1-1 to cn-1,..., C1-m to cn-m. However, the characteristic difference between the earth station facilities b1 to bn is limited to compensation only for two stations having the same elevation angle difference from the artificial satellite a. Therefore, in the measurement method of the second embodiment, since the reception levels are the same at the intersections of the cut patterns c3-1, c1-2, and d2 indicated by Δ shown in FIG. 9, the earth station facilities b1, b2, b3 It is possible to compensate for the characteristics of The measured elevation cut pattern c1-2 and azimuth cut pattern d2 are shown in FIG. In the figure, Δ is an angle corresponding to the intersection of each of c1-2 and d2, and the characteristics of the earth station facilities b1 and b2 can be compensated by canceling these reception level differences.
本発明の第3および第4の実施形態に係る衛星搭載アンテナ測定方法は、本発明の第1および第2の実施形態に係る搭載アンテナ測定方法において、互いに直交するピッチ軸とロール軸および仰角と方位角を入れ替えたものである。 The satellite mounted antenna measurement method according to the third and fourth embodiments of the present invention is the same as the mounted antenna measurement method according to the first and second embodiments of the present invention, and includes a pitch axis, a roll axis, and an elevation angle orthogonal to each other. The azimuth is switched.
また、本発明の第1の実施形態および第3の実施形態の方法を実施し、両者の測定結果の平均を取ることによって、方位角誤差と仰角誤差の双方を補償することもできる。 Moreover, both the azimuth angle error and the elevation angle error can be compensated by carrying out the methods of the first and third embodiments of the present invention and taking the average of the measurement results of both.
本発明の第5の実施形態に係る衛星搭載アンテナパタン測定方法は、受信アンテナの測定方法を実現する。そのため、信号の方向を変え、地球局設備b1〜bnから送信し、人工衛星aにて受信レベルを測定するものである。この場合、地球局設備b1〜bnで異なる周波数で信号を送信する必要があるが、衛星搭載アンテナの動作周波数帯はマイクロ波・ミリ波帯(GHzオ−ダ)であり、一方、分離可能な周波数帯は隣接ch間の周波数帯であるkhzオ−ダであるため、評価の際の周波数特性は無視しても構わないレベルと言える。 The satellite mounted antenna pattern measuring method according to the fifth embodiment of the present invention realizes a receiving antenna measuring method. Therefore, the direction of the signal is changed, transmitted from the earth station facilities b1 to bn, and the reception level is measured by the artificial satellite a. In this case, it is necessary to transmit signals at different frequencies in the earth station facilities b1 to bn. However, the operating frequency band of the satellite-mounted antenna is a microwave / millimeter wave band (GHz order), but can be separated. Since the frequency band is a khz order which is a frequency band between adjacent channels, it can be said that the frequency characteristics at the time of evaluation can be ignored.
また、以上述べた実施形態は全て本発明を例示的に示すものであって限定的に示すものではなく、本発明は他の種々の変形態様及び変更態様で実施することができる。従って本発明の範囲は特許請求の範囲及びその均等範囲によってのみ規定されるものである。 Moreover, all the embodiment described above shows the present invention exemplarily, and does not limit the present invention, and the present invention can be implemented in other various modifications and changes. Therefore, the scope of the present invention is defined only by the claims and their equivalents.
a 人工衛星
b1〜bn 地球局設備
c1−1〜c1−m 地球局設備b1にて得られるロール角設定時の方位角カットパタン
cn−1〜cn−m 地球局設備bnにて得られるロール角設定時の方位角カットパタン
d1〜dn 地球局設備b1〜bnにて得られる仰角カットパタン
a Artificial satellites b1 to bn Earth station equipment c1-1 to c1-m Azimuth cut patterns obtained when the roll angle is set in the earth station equipment b1 cn-1 to cn-m Roll angles obtained from the earth station equipment bn Azimuth cut pattern at the time of setting d1 to dn Elevation angle cut pattern obtained by the earth station facilities b1 to bn
Claims (5)
人工衛星から一定電力の信号を該衛星搭載アンテナより出力し、該衛星搭載アンテナのロール軸周りの角度を一定値に設定し、ピッチ軸周りの角度を走査し、該衛星搭載アンテナの出力信号を該地球局設備にて受信電力レベルを測定し、該人工衛星のロール軸の設定角度および地球局設備の設置位置から、該人工衛星からの仰角オフセット量の異なる方位角カットパタンを該地球局設備と同数個生成する第1の生成ステップと、
該人工衛星のロール軸の設定角度を一定の増減分で順次変え、前記第1の生成ステップを繰り返すことにより、複数の方位角カットパタンを生成する第2の生成ステップと、
を有し、前記一定の増減分と、該複数の地球局設備の何れか2つの該人工衛星からの仰角差が等しい角度であることを特徴とする衛星搭載アンテナパタン測定方法。 In a method of measuring a two-dimensional antenna pattern of a satellite-mounted antenna using a plurality of earth station facilities,
A constant power signal is output from the satellite-mounted antenna from the artificial satellite, the angle around the roll axis of the satellite-mounted antenna is set to a constant value, the angle around the pitch axis is scanned, and the output signal of the satellite-mounted antenna is A reception power level is measured by the earth station facility, and an azimuth cut pattern having a different elevation angle offset amount from the artificial satellite is determined from the roll axis setting angle of the satellite and the installation position of the earth station facility. A first generation step of generating the same number as
A second generation step of generating a plurality of azimuth cut patterns by sequentially changing the set angle of the roll axis of the artificial satellite by a constant increase / decrease and repeating the first generation step;
The satellite-mounted antenna pattern measuring method, wherein the constant increase / decrease amount is equal to an elevation angle difference between any two satellites of the plurality of earth station facilities.
人工衛星から一定電力の信号を該衛星搭載アンテナより出力し、該衛星搭載アンテナのピッチ軸周りの角度を一定値に設定し、ロール軸周りの角度を走査し、該衛星搭載アンテナの出力信号を該地球局設備にて受信電力レベルを測定し、該人工衛星のピッチ軸の設定角度および地球局設備の設置位置から、該人工衛星からの方位角オフセット量の異なる仰角カットパタンを該地球局設備と同数個生成する第1の生成ステップと、
該人工衛星のピッチ軸の設定角度を一定の増減分で順次変え、前記第1の生成ステップを繰り返すことにより、複数の仰角カットパタンを生成する第2の生成ステップと、
を有し、前記一定の増減分と、該複数の地球局設備の何れか2つの該人工衛星からの方位角差が等しい角度であることを特徴とする衛星搭載アンテナパタン測定方法。 In a method of measuring a two-dimensional antenna pattern of a satellite-mounted antenna using a plurality of earth station facilities,
A constant power signal is output from the satellite-mounted antenna from the artificial satellite, the angle around the pitch axis of the satellite-mounted antenna is set to a constant value, the angle around the roll axis is scanned, and the output signal of the satellite-mounted antenna is The earth station equipment measures the received power level, and calculates the elevation angle cut patterns having different azimuth offset amounts from the artificial satellite from the set angle of the pitch axis of the satellite and the installation position of the earth station equipment. A first generation step of generating the same number as
A second generation step of generating a plurality of elevation angle cut patterns by sequentially changing the set angle of the pitch axis of the artificial satellite by a constant increase / decrease and repeating the first generation step;
A satellite-mounted antenna pattern measuring method, characterized in that the constant increase / decrease and an azimuth difference between any two satellites of the plurality of earth station facilities are equal.
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