JPH0728242B2 - Frequency signal generator - Google Patents

Frequency signal generator

Info

Publication number
JPH0728242B2
JPH0728242B2 JP63308900A JP30890088A JPH0728242B2 JP H0728242 B2 JPH0728242 B2 JP H0728242B2 JP 63308900 A JP63308900 A JP 63308900A JP 30890088 A JP30890088 A JP 30890088A JP H0728242 B2 JPH0728242 B2 JP H0728242B2
Authority
JP
Japan
Prior art keywords
frequency
signal
receiver
output
pilot
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP63308900A
Other languages
Japanese (ja)
Other versions
JPH02155317A (en
Inventor
新一 大谷
祥三 中里
修 竹田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NEC Corp
Original Assignee
NEC Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by NEC Corp filed Critical NEC Corp
Priority to JP63308900A priority Critical patent/JPH0728242B2/en
Publication of JPH02155317A publication Critical patent/JPH02155317A/en
Publication of JPH0728242B2 publication Critical patent/JPH0728242B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は主として人工衛星搭載用通信機器,特に中継器
の構成方法に関し,この中継器を構成する送・受信機の
局部発振器の周波数を高安定かつ任意に変化させること
ができる周波数信号発生装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial field of application] The present invention mainly relates to a method for constructing a communication device mounted on an artificial satellite, in particular, a repeater, in which the frequency of a local oscillator of a transmitter / receiver constituting this repeater is increased. The present invention relates to a frequency signal generator that can be stably and arbitrarily changed.

〔従来の技術〕[Conventional technology]

従来、人工衛星搭載用中継機においては、周波数信号発
生源として周波数シンセサイザを備えている。この周波
数シンセサイザは、パイロット受信機の位相同期ル−プ
(PLL)内の電圧制御発振器(VCO)の出力を基準信号源
とし、このVCO出力を所要の局発信号まで逓倍する様な
構成を採っていた。
Conventionally, a satellite-mounted repeater has a frequency synthesizer as a frequency signal generation source. This frequency synthesizer uses the output of the voltage controlled oscillator (VCO) in the phase locked loop (PLL) of the pilot receiver as a reference signal source and multiplies this VCO output to the required local oscillator signal. Was there.

〔発明が解決しようとする課題〕[Problems to be Solved by the Invention]

上述した周波数信号発生方式では、次の欠点が有る。 The frequency signal generating method described above has the following drawbacks.

(1)VCO出力の位相雑音が少くとも逓倍次数(n)の2
0lognデシベル分だけ逓倍器出力で劣化する。
(1) The phase noise of the VCO output is at least 2 of the multiplication order (n)
Degraded by 0logn decibels in the multiplier output.

(2)VCO出力の周波数は,パイロット受信機の受信可
能周波数範囲の約1/m(m:パイロット受信機の第1局発
周波数とVCO出力の周波数との比)程度の範囲で可変で
あるが、この範囲より大幅な周波数変化幅を得ることが
困難である。
(2) The frequency of the VCO output is variable within a range of about 1 / m of the receivable frequency range of the pilot receiver (m: ratio of the frequency of the first station of the pilot receiver to the frequency of the VCO output). However, it is difficult to obtain a large frequency change range beyond this range.

〔課題を解決するための手段〕[Means for Solving the Problems]

本発明は、地上局から送信された周波数安定度の高いパ
イロット信号を受信する為の位相同期ル−プ(PLL)型
受信機において、この受信機のPLLを構成しているVCOの
出力を基準信号として入力されるディジタル制御型周波
数シンセサイザ群を備え、この周波数シンセサイザ群の
一系統の出力を前記パイロット受信機の第1局発信号源
の基準信号として接続するようにしたものである。
The present invention, in a phase-locked loop (PLL) type receiver for receiving a pilot signal with high frequency stability transmitted from a ground station, is based on the output of the VCO that constitutes the PLL of this receiver. A digital control type frequency synthesizer group input as a signal is provided, and an output of one system of this frequency synthesizer group is connected as a reference signal of a first station signal source of the pilot receiver.

〔実施例〕〔Example〕

第1図は本発明の一実施例の機能系統図である。パイロ
ット受信機1は位相比較器11、逓倍器12を有し、地上局
から送信されたKaバンドのパイロット信号を、逓倍器12
で得られるKaバンドの局発信号によりSバンドの中間周
波数へ変換する。又、パイロット受信機2は位相比較器
21〜23、逓倍器24〜26、VCXO27を有し、これらをPLL回
路構成とすることによりSバンド信号に位相同期する機
能を有する。PLL回路内のVCXO27の出力はシンセサイザ
部3の基準信号として分周器31へ接続される。
FIG. 1 is a functional system diagram of an embodiment of the present invention. The pilot receiver 1 has a phase comparator 11 and a multiplier 12, and a Ka band pilot signal transmitted from a ground station is transmitted to the multiplier 12
Convert to the intermediate frequency of the S band by the local signal of the Ka band obtained in. Also, the pilot receiver 2 is a phase comparator.
It has 21 to 23, multipliers 24 to 26, and VCXO27, and these have a function of phase-locking to the S band signal by forming a PLL circuit configuration. The output of the VCXO 27 in the PLL circuit is connected to the frequency divider 31 as a reference signal of the synthesizer section 3.

シンセサイザ部3は分周器31,位相比較器32,ループフィ
ルタ33,VCO34及びプリンスケーラ35で構成され,VCO34の
出力はパイロット受信機1の局発信号源として,逓倍器
12の入力に接続される。
The synthesizer unit 3 is composed of a frequency divider 31, a phase comparator 32, a loop filter 33, a VCO 34 and a prince scaler 35. The output of the VCO 34 serves as a local oscillator signal source of the pilot receiver 1 and a multiplier.
Connected to 12 inputs.

なお,第1図中,各逓倍器,分周器に付された数字はそ
れぞれ逓倍数,分周数を表わし,周波数を表わす数値も
一例であって本発明はこれに制限されるものではない。
It should be noted that in FIG. 1, the numbers attached to the multipliers and the frequency dividers respectively represent the multiplication number and the frequency division number, and the numerical values representing the frequency are also examples, and the present invention is not limited thereto. .

また,図ではシンセサイザ部3はパイロット受信機1の
局発信号を得るための手段として1つだけ図示している
が,これはVCXO27の出力を並列に受けるように複数個備
えられ,他の部位の様々な周波数信号源として利用され
る。
Further, in the figure, only one synthesizer unit 3 is shown as a means for obtaining the local oscillator signal of the pilot receiver 1, but a plurality of synthesizer units 3 are provided so as to receive the output of the VCXO27 in parallel, and other parts are provided. Are used as various frequency signal sources.

本発明により得られる周波数信号は,パイロット信号を
全ての位相関係が同期状態(コヒーレント)にある信号
源により分周・逓倍した局発源となっており,以下に示
す特徴が有る。
The frequency signal obtained by the present invention is a local oscillation source obtained by dividing / multiplying a pilot signal by a signal source in which all phase relationships are in a synchronous state (coherent), and has the following characteristics.

(1)パイロット信号の周波数安定度及び位相雑音レベ
ルにパイロット受信機1及びパイロット受信機2の局発
系が同期するため,VCXO27出力の周波数安定度及び位相
雑音レベルは少くともシンセサイザ部3,及び逓倍器12の
総合逓倍次数分だけ改善される。従って,シンセサイザ
部3の出力では非常に安定度の高い信号を得ることがで
きる。
(1) Since the local oscillation system of the pilot receiver 1 and pilot receiver 2 is synchronized with the frequency stability and phase noise level of the pilot signal, the frequency stability and phase noise level of the VCXO27 output are at least the synthesizer section 3, and It is improved by the total multiplication order of the multiplier 12. Therefore, a very stable signal can be obtained from the output of the synthesizer section 3.

(2)プリスケーラ35の分周比を変えることにより,高
安定な信号源の周波数を大幅に変化させることができ
る。(例えば,±10MHz程度) (3)パイロット信号の周波数を動かすことにより,シ
ンセサイザ部3の出力を連続的に動かすことができる。
(2) By changing the division ratio of the prescaler 35, the frequency of the highly stable signal source can be changed significantly. (For example, about ± 10 MHz) (3) By moving the frequency of the pilot signal, the output of the synthesizer unit 3 can be continuously moved.

〔発明の効果〕〔The invention's effect〕

以上説明してきたように本発明によれば,位相雑音を改
善して周波数安定度の高い周波数信号を得ることがで
き,しかも周波数の可変幅を従来のものに比して大幅に
とることができる。
As described above, according to the present invention, it is possible to improve the phase noise and obtain a frequency signal with high frequency stability, and moreover, the variable width of the frequency can be largely taken as compared with the conventional one. .

【図面の簡単な説明】[Brief description of drawings]

第1図は本発明の一実施例の機能系統図である。 1,2……パイロット受信機,3……シンセサイザ部,31……
分周器,32……位相比較器,33……ループフィルタ,34…
…VCO,35……プリスケーラ。
FIG. 1 is a functional system diagram of an embodiment of the present invention. 1,2 …… Pilot receiver, 3 …… Synthesizer section, 31 ……
Frequency divider, 32 …… Phase comparator, 33 …… Loop filter, 34…
… VCO, 35 …… Prescaler.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】地上局から送信されたパイロット信号を受
信する為の位相同期ループ型受信機において,該受信機
の位相同期ループを構成している電圧制御発振器の出力
を基準信号として供給されるディジタル制御型周波数シ
ンセサイザ群を備え,該周波数シンセサイザ群の一系統
の出力を前記パイロット受信機の第1局発信号源の基準
信号として接続したことを特徴とする周波数信号発生装
置。
1. A phase locked loop type receiver for receiving a pilot signal transmitted from a ground station, wherein the output of a voltage controlled oscillator constituting a phase locked loop of the receiver is supplied as a reference signal. A frequency signal generator comprising a digital control type frequency synthesizer group, and an output of one system of the frequency synthesizer group is connected as a reference signal of a first station signal source of the pilot receiver.
JP63308900A 1988-12-08 1988-12-08 Frequency signal generator Expired - Lifetime JPH0728242B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63308900A JPH0728242B2 (en) 1988-12-08 1988-12-08 Frequency signal generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63308900A JPH0728242B2 (en) 1988-12-08 1988-12-08 Frequency signal generator

Publications (2)

Publication Number Publication Date
JPH02155317A JPH02155317A (en) 1990-06-14
JPH0728242B2 true JPH0728242B2 (en) 1995-03-29

Family

ID=17986621

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63308900A Expired - Lifetime JPH0728242B2 (en) 1988-12-08 1988-12-08 Frequency signal generator

Country Status (1)

Country Link
JP (1) JPH0728242B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7327197B2 (en) * 2005-10-20 2008-02-05 Honeywell International, Inc. Radiation hardened phase locked loop

Also Published As

Publication number Publication date
JPH02155317A (en) 1990-06-14

Similar Documents

Publication Publication Date Title
JP2526847B2 (en) Digital wireless telephone
US5065408A (en) Fractional-division synthesizer for a voice/data communications systems
JPH01151823A (en) Frequency synthesizer
US4720688A (en) Frequency synthesizer
US4303893A (en) Frequency synthesizer incorporating digital frequency translator
GB1253929A (en) Improvements in and relating to a frequency synthesizer
US4791387A (en) Microwave band frequency synthesizer
JPH0728242B2 (en) Frequency signal generator
JPH0834589B2 (en) Sampling clock generator
RU195894U1 (en) Frequency synthesizer
EP0213636A2 (en) Frequency synthesizer of a phase-locked type with a sampling circuit
JPH0728258B2 (en) Signal generator
SU746909A1 (en) Frequency-and-phase manipulated oscillation shaper
JPS5918757Y2 (en) Frequency synthesizer using PLL circuit
JPS5676640A (en) Receiver of frequency synthesizer system
JPS61261926A (en) Frequency synthesizer
JPH0580848B2 (en)
JPS5776930A (en) Frequency shift signal generating system using pll
SU758529A1 (en) Device for automatic tuning of frequency
SU862362A1 (en) Digital frequency synthesizer
SU389608A1 (en) FREQUENCY SYNTHESIZER
JPH0728256B2 (en) Signal generator
JPH06224957A (en) Radio transmitter
JPH03157019A (en) Frequency synthesizer
JPS5856293B2 (en) Auxiliary signal input method for multidirectional communication network