JPS60252097A - Control system for automatic steering gear - Google Patents
Control system for automatic steering gearInfo
- Publication number
- JPS60252097A JPS60252097A JP59107496A JP10749684A JPS60252097A JP S60252097 A JPS60252097 A JP S60252097A JP 59107496 A JP59107496 A JP 59107496A JP 10749684 A JP10749684 A JP 10749684A JP S60252097 A JPS60252097 A JP S60252097A
- Authority
- JP
- Japan
- Prior art keywords
- course
- output
- deltad
- angle
- ship
- 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.)
- Granted
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
Description
【発明の詳細な説明】
船舶の自動操舵装置における制御情報として、目的地方
位と自船の針路すなわも航行方位との角度差を用いる場
合、同情報のセンサー(例えばロランC受信機)からの
データは、ふらつきおよび反応遅れから制御過多を起し
、船舶は蛇行やコースよりはずれる現象を伴う。このた
め一般的には、データのふらつぎによる蛇行を防ぐため
、曲記角い方法がとられる。[Detailed Description of the Invention] When using the angular difference between the destination position and the own ship's course or navigation direction as control information in a ship's automatic steering system, the same information is obtained from a sensor (for example, a Loran C receiver). The data shows that over-control occurs due to wandering and delayed reaction, and the ship meanderes and deviates from the course. For this reason, in order to prevent meandering due to data fluctuations, a method of notation is generally used.
しかしコースはずれについては、コースのずれ量の絶対
量管理が行なわれていないため、潮流等の影響で航路は
弓形となりやすい。またコースずれの情報のみをセンサ
ーから得て、船がコースからはずれた場合にコースに復
帰する方向に転舵する方法もあるが、この場合には舵角
が目的地の方向でなく、コース上に向くためコースを横
切る形での激しい蛇行が発生しやすい欠点がある゛。However, as there is no absolute amount of course deviation control, the course tends to become arched due to the effects of tidal currents, etc. There is also a method of obtaining only information on course deviation from sensors and steering the ship in the direction of returning to the course if it deviates from the course, but in this case the rudder angle is not in the direction of the destination but on the course. The disadvantage is that it tends to cause severe meandering across the course.
本発明は制御情報として、目的地方位と航行方位との角
度差およびコースずれ量を用いるもので、前記欠点を解
消し船舶の運行に当り、安全かつ省燃費に極めて効果の
ある自動操舵装置の制御方式を提供せんとするものであ
る。The present invention uses the angular difference between the destination position and the navigation direction and the amount of course deviation as control information, and eliminates the above-mentioned drawbacks and provides an automatic steering system that is extremely effective in safe and fuel-efficient operation of ships. The purpose is to provide a control method.
以下図面により詳細に説明する。第1図は本発明の説明
図、第2図は本発明の実施例のブロック図で、1は船舶
の出発点、2は目的地点で3はこれらを結ぶ航路即ちコ
ースである。4はある時点における船舶の位置を示し、
5はこの時の目的地方位、6はこの航行方位である。こ
の5および6は、船舶位置から真北Nを望む方位に対す
る角度αおよびβで示す。△Dは図から分るように、a
とβとの角度差である。また士△dは△Dのふらつき幅
である。This will be explained in detail below with reference to the drawings. FIG. 1 is an explanatory diagram of the present invention, and FIG. 2 is a block diagram of an embodiment of the present invention, in which 1 is a starting point of a ship, 2 is a destination point, and 3 is a route or course connecting these points. 4 indicates the position of the ship at a certain point in time;
5 is the destination position at this time, and 6 is the current navigation direction. These 5 and 6 are indicated by angles α and β with respect to the azimuth looking toward due north N from the ship's position. As can be seen from the figure, △D is a
is the angular difference between and β. Further, Δd is the fluctuation width of ΔD.
上記のaおよびβは、第2図のロランC受信機等の航法
装置10から得られるが、これは時時刻刻変動するので
、自動操舵装置の航路修正すべき一定時間毎に、それ以
前のデータから、11なる算出回路でβとαとの差の平
均値(±ΔD)を、また12の算出回路でそのふらつき
幅(±Δd)を算出する。なおふらつき幅は、最大およ
び最小値からめた範囲または分散等を使用する。The above a and β are obtained from the navigation device 10 such as the Loran C receiver shown in FIG. From the data, an 11 calculation circuit calculates the average value (±ΔD) of the difference between β and α, and a 12 calculation circuit calculates the fluctuation width (±Δd). Note that the range or variance between the maximum and minimum values is used as the fluctuation width.
このようにして得られたΔDおよび△dは、13なる出
力条件判断回路でΔD〉Δdのときは、△Dを、またΔ
D≦△dのときは、0を出力し16の出力回路に印加す
る。ΔD and Δd obtained in this way are determined by the output condition determination circuit 13. When ΔD>Δd, ΔD and Δ
When D≦△d, 0 is output and applied to 16 output circuits.
一方第1図で△しは船舶4がコース3がらのずれ量であ
り、これもロランC等の航法装置10かち得られる。こ
のΔしはコースずれによる舵角修正量を制限するため、
使用者等が設定する定数L(コースずれの許容範囲)と
比較し、14なる検出回路および15なる出力条件判断
回路で、L≦ししのときは、コースに復帰する方向への
舵角として、12で得られたΔdを、またし〉△しのと
きはOを出力し、前記16に印加される。16の出力回
路は、上記13.15の出力によって第1表の如き出力
を、修正舵角出力とし、操舵装置17に印加し航路修正
が行われる。On the other hand, in FIG. 1, △ indicates the amount of deviation of the ship 4 from the course 3, which can also be obtained from the navigation device 10 such as Loran C. This delta limits the amount of steering angle correction due to course deviation, so
The detection circuit 14 and the output condition judgment circuit 15 compare the constant L (tolerable range of course deviation) set by the user, etc., and when L≦I, the steering angle is determined in the direction of returning to the course. , 12, and when >△, outputs O, which is applied to 16. The output circuit 16 uses the output shown in Table 1 as a corrected steering angle output based on the output 13.15, and applies the output to the steering device 17 to correct the course.
第1表
次に第3図は、本発明の他の実施例のブロック図である
。この実施例は、前記自船舶4の目的地方位5と航行方
位6の差のふらつき幅(±Δd)の代りに、経験的にめ
た一定値θを用いるものである。Table 1 and FIG. 3 are block diagrams of other embodiments of the present invention. In this embodiment, instead of the fluctuation width (±Δd) of the difference between the destination position 5 and the navigational direction 6 of the host vessel 4, a constant value θ determined empirically is used.
二のため坑2MのΔd箆S」、同誌12が不要となるの
で、全体の構成が簡略化される特長がある。Since the second shaft 2M Δd S and the magazine 12 are not required, the overall structure is simplified.
なお、第3図の18は上記一定値θの設定回路であり、
この出力は、13および15にも印加されるので、13
においては、ΔDとθとの比較が行われ、15ではL≦
Δしのときθが、復帰舵角の出力となる。In addition, 18 in FIG. 3 is a setting circuit for the above-mentioned constant value θ,
This output is also applied to 13 and 15, so 13
In , a comparison is made between ΔD and θ, and in 15, L≦
When Δ, θ becomes the output of the return steering angle.
したがって16よりの出力は、@2表の如くになる。Therefore, the output from 16 will be as shown in table @2.
第2表
以上説明したように本発明は、自動操舵装置の制御情報
として、目的地方位と航行方位の角度差およびコースず
れ量の両者を併用するとともに、(、)コースずれによ
る舵角修正に対し制限を設ける、(b)目的地方位と航
行方位の角度差情報と、コースずれ情報との制御切換角
度に、しきい値を設ける。(c)このしきい値は、角度
差情報のふらっぎ幅を用いるようにしたものである。Table 2 As explained above, the present invention uses both the angular difference between the destination position and the navigation direction and the amount of course deviation as control information for the automatic steering system, and also () corrects the steering angle due to course deviation. (b) A threshold value is set for the control switching angle between the angular difference information between the destination position and the navigation direction and the course deviation information. (c) This threshold value uses the fluctuation width of the angle difference information.
このためコースはずれすることなく、がっ、コース上で
の蛇行角度を最小限になし得るので、従来の如く角度情
報またはコースはずれ情報の一方のみによる制御よりも
、円滑な自動操舵が可能となり、潮流等の影響なく、安
全かつ省燃費の面でも極めて効果ある制御方式が提供で
きるものである。Therefore, the meandering angle on the course can be minimized without deviating from the course, so smoother automatic steering is possible than conventional control based only on angle information or course deviation information. It is possible to provide a control method that is extremely effective in terms of safety and fuel efficiency, without being affected by tidal currents, etc.
第1図は本発明の説明図、第2図は本発明の実施例のブ
ロック図、第3図は本発明の他の実施例のブロック図で
ある。
1・・・出発地点、2・・・目的地点、3・・・コース
、4・・・船舶位置、5・・・目的地方位、6・・・航
行方位、10・・・航行装置、11・12・・・算出回
路、13・15・・・出力条件判断回路、14・・・検
出回路、16・・・出力回路、17・・・操舵装置、1
ト・・一定値設定回路、出願人 株式会社 光電製作所
代表取締役 伊 藤 良 励1
図面の浄書(内容に変更なし)
オ 2図
手続補正者(自発)
昭和59年7月 t 日
特許庁長官 殿
]、事件の表示
特願昭59− /θ7グq6
2、発明の名称
自動捏舵装置の制御方式
3、補正をする者
事件との関係 特許出願人
〒141 東京部品用区上大崎2−10−45明細書・
図面
5、補正の内容FIG. 1 is an explanatory diagram of the present invention, FIG. 2 is a block diagram of an embodiment of the invention, and FIG. 3 is a block diagram of another embodiment of the invention. 1... Departure point, 2... Destination point, 3... Course, 4... Ship position, 5... Destination position, 6... Navigation direction, 10... Navigation device, 11・12...Calculation circuit, 13.15...Output condition judgment circuit, 14...Detection circuit, 16...Output circuit, 17...Steering device, 1
G. Constant value setting circuit, Applicant: Koden Seisakusho Co., Ltd. Representative Director Ryo Ito 1. Engraving of the drawings (no changes to the contents). 2. Procedural amendment of drawings (on his own initiative). July 1980. t. Mr. Commissioner of the Japanese Patent Office. ], Indication of the case Patent application 1987-/θ7guq6 2, Title of the invention Control method for automatic steering device 3, Person making the amendment Relationship to the case Patent applicant 2-10 Kamiosaki, Tokyo Parts Industry Ward, 141 -45 statement/
Drawing 5, contents of correction
Claims (2)
行う自動操舵装置において、人力されtこ目的地方位と
自船の航行方位より、一定時間当りの目的地方位と航行
方位との差の平均値(±△D)および、このふらつき幅
(±△d)を算出する第1の過程と、 前記第1の過程によりまったΔDと△dとを比較し、±
ΔD〉±△dが成立するときのみ、修正舵角として△D
を出力する第2の過程と、入力された自船位置のコース
よりのはずれ量(Δし)と、使用者等が設定した定数(
L)を比較し、△し≧Lが成立するときのみ、コースへ
の復帰角度として、第1の過程で得られたΔdを出力す
る第3の過程と、 前記第2および第3の過程から得られた△Dおあるとぎ
は、△Dを、また、△D出力がなく、Δd出力があると
きは△d出力を、 また△DおよびΔd出力の双方がないときは0出力を、
舵角出力とする第4の過程と、前記第4の過程で得られ
た出力を操舵装置に与へる第5の過程とを有することを
特徴とする自動操舵装置の制御方式。(1) In the automatic steering system, which is operated by obtaining control information from a ship's navigation system such as Loran C, the destination position and navigation direction for a certain period of time are determined manually based on the destination position and the own ship's navigation direction. The first process of calculating the average value of the difference (±△D) and the fluctuation width (±△d) is compared with ΔD and △d determined by the first process, and ±
Only when ΔD〉±△d holds true, use ΔD as the corrected steering angle.
The second process outputs the amount of deviation from the input own ship position from the course (Δ) and the constant (Δ) set by the user etc.
L), and only when △≧L holds true, a third process outputs Δd obtained in the first process as the return angle to the course; and from the second and third processes. The obtained △D output is △D, and when there is no △D output and Δd output, △d output, and when both △D and Δd output are absent, 0 output,
A control system for an automatic steering system, comprising a fourth process of outputting a steering angle, and a fifth process of applying the output obtained in the fourth process to a steering system.
位の差のふらつき幅(±Δd)を、経験的にめた一定値
(θ)とすることを特徴とする特許請求範囲第1項記載
の自動操舵装置の制御方式。(2) In the above (1), the fluctuation range (±Δd) of the difference between the destination position and the own ship's navigational direction is set to a constant value (θ) determined empirically. A control method for the automatic steering device according to item 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59107496A JPS60252097A (en) | 1984-05-29 | 1984-05-29 | Control system for automatic steering gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP59107496A JPS60252097A (en) | 1984-05-29 | 1984-05-29 | Control system for automatic steering gear |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS60252097A true JPS60252097A (en) | 1985-12-12 |
| JPH0417837B2 JPH0417837B2 (en) | 1992-03-26 |
Family
ID=14460679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP59107496A Granted JPS60252097A (en) | 1984-05-29 | 1984-05-29 | Control system for automatic steering gear |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60252097A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6328794A (en) * | 1986-07-23 | 1988-02-06 | Furuno Electric Co Ltd | Autopilot device |
| JP2012017058A (en) * | 2010-07-09 | 2012-01-26 | Marol Ltd | Control device for hull, control program for hull, and automatic steering system incorporating the control program for hull |
| JP2014148271A (en) * | 2013-02-01 | 2014-08-21 | Honda Motor Co Ltd | Controller for outboard engine |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5779408A (en) * | 1980-11-05 | 1982-05-18 | Tokyo Keiki Co Ltd | Automatic navigating device |
-
1984
- 1984-05-29 JP JP59107496A patent/JPS60252097A/en active Granted
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5779408A (en) * | 1980-11-05 | 1982-05-18 | Tokyo Keiki Co Ltd | Automatic navigating device |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6328794A (en) * | 1986-07-23 | 1988-02-06 | Furuno Electric Co Ltd | Autopilot device |
| JP2012017058A (en) * | 2010-07-09 | 2012-01-26 | Marol Ltd | Control device for hull, control program for hull, and automatic steering system incorporating the control program for hull |
| JP2014148271A (en) * | 2013-02-01 | 2014-08-21 | Honda Motor Co Ltd | Controller for outboard engine |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0417837B2 (en) | 1992-03-26 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4866627A (en) | Direction finder | |
| US5060175A (en) | Measurement and control system for scanning sensors | |
| DE3279088D1 (en) | High accuracy navigating apparatus with step-driven projected chart | |
| US5349531A (en) | Navigation apparatus using a global positioning system | |
| WO1992005505A1 (en) | Course-to-steer navigation system | |
| JPS60252097A (en) | Control system for automatic steering gear | |
| US3280781A (en) | Auto-pilot system | |
| US4116057A (en) | Pendulous induction compass transmitter with means to compensate for heading errors in turns due to the vertical component of the Earth's magnetic field and due to two cycle error | |
| RU2144884C1 (en) | Ship's motion automatic control equipment | |
| US3737635A (en) | Constant line of position navigation system | |
| JPS6234000B2 (en) | ||
| RU2098322C1 (en) | Complex compass system | |
| JPS6233998B2 (en) | ||
| JPS6210877B2 (en) | ||
| JPH0325094A (en) | How to berth a ship | |
| JPS61128120A (en) | Automatic navigating apparatus | |
| JP4459017B2 (en) | Moving body position calculating apparatus and calculating method | |
| JPH0283411A (en) | Method for determining attitude of space flight body | |
| JP2590608B2 (en) | Vehicle running direction calculation device | |
| JP3427944B2 (en) | Trajectory tracking positioning control method | |
| JPH0425200B2 (en) | ||
| JPH0414287B2 (en) | ||
| JPS6252475A (en) | System for automatically tracking satellite | |
| JPH0363523A (en) | Autonomous navigation guidance device | |
| JPS6233999B2 (en) |