JPH06247393A - Automatic airship control device with automated obstacle avoidance device - Google Patents

Automatic airship control device with automated obstacle avoidance device

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Publication number
JPH06247393A
JPH06247393A JP5658593A JP5658593A JPH06247393A JP H06247393 A JPH06247393 A JP H06247393A JP 5658593 A JP5658593 A JP 5658593A JP 5658593 A JP5658593 A JP 5658593A JP H06247393 A JPH06247393 A JP H06247393A
Authority
JP
Japan
Prior art keywords
airship
automatic
obstacle
control device
distance
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.)
Pending
Application number
JP5658593A
Other languages
Japanese (ja)
Inventor
Hideo Taira
秀夫 平
Hiromitsu Masaki
裕光 正木
Hiroo Kusaya
大郎 草谷
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.)
SKY PIA KK
Original Assignee
SKY PIA KK
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 SKY PIA KK filed Critical SKY PIA KK
Priority to JP5658593A priority Critical patent/JPH06247393A/en
Publication of JPH06247393A publication Critical patent/JPH06247393A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To enhance stability of a device which effects automatic navigation based on a preinputted navigation program by preferring automatic obstacle avoidance control to the automatic navigation program if an obstacle is detected on course. CONSTITUTION:An obstacle detecting device comprises ultrasonic sensors 2a-7a each of which has directivity and transmits and receives ultrasonic waves, and provided respectively at the front and rear portions, right and left middle portions, and upper and lower portions of an airship, and distance measuring circuits 2b-7b each of which calculates the distance to an obstacle from the time from transmission to reception at each sensor. The detection results of the detecting system are inputted to a control unit 9 and compared at comparison circuits with the dangerous distance to the obstacle which is prestored in a storage device, and a judging circuit for the direction of escape determines the direction of escape from the comparison results. A signal for preferring automatic airship control is outputted to a CPU according to the judgment result and an input method is changed, and a control portion A comprising a pusher 9 and a bow 10 is controlled so that the airship takes escaping action.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、無人飛行船の操船技術
の改良に関するもので、特にコンピュータに記憶された
航法プログラムに基づき操船する飛行船において、超音
波センサーを用いて障害物を検知し、障害物が存在する
時に航法プログラムに優先して回避行動をとらせること
により無人自動操船を可能とするものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improvement in unmanned airship maneuvering technology, and in particular, in an airship maneuvering based on a navigation program stored in a computer, an obstacle is detected by using an ultrasonic sensor to detect an obstacle. It enables unmanned automatic marine vessel maneuvering by giving priority to the navigation program and taking avoidance action when an object exists.

【0002】[0002]

【従来技術】従来の無人飛行船の操船技術としては、地
上に移動無線局を置き、該オペレータから飛行船の無線
局に送信し、該送信信号に基づき操作部を操作して飛行
船を右旋回、左旋回、上昇又は下降させることにより飛
行させるラジコン操船技術等が知られている。
2. Description of the Related Art As a conventional unmanned airship maneuvering technique, a mobile radio station is placed on the ground, the operator transmits to the radio station of the airship, and the operating unit is operated based on the transmission signal to turn the airship to the right, A radio-controlled marine vessel maneuvering technique for flying by turning left, ascending or descending is known.

【0003】[0003]

【発明が解決しようとする課題】しかしながらかかる従
来の無線操船方式の場合には、常に飛行船に搭乗したつ
もりになり無線にて飛行船をコントロールしなければな
らないことから、無線操縦者に極度の緊張を与えるため
に長時間の飛行には不向きであった。また、無線飛行さ
せるためには様々な状況に応じて判断・対応しなければ
ならないため、無線操縦オペレータの育成にかなりの訓
練を要している。さらに、都市部の飛行においては超高
層ビル等が建ち並んだり、地上を様々な電波が行き交う
関係から、混信や電波障害などにより一時的に操船不能
になったり地上構造物に接触するおそれがある。そこで
本発明はかかる従来技術の欠点に鑑みなされたもので、
オペレータ訓練の必要がなく、混信、電波障害になって
も安全に飛行させることのできる飛行船の自動操船装置
を提供することを目的とする。
However, in the case of such a conventional wireless marine vessel maneuvering system, since it is always intended to board an airship and the airship must be controlled by radio, the radio operator is extremely tense. It was not suitable for a long flight to give. In addition, since it is necessary to judge and respond to various situations in order to carry out wireless flight, considerable training is required to train wireless pilot operators. Further, in a flight in an urban area, skyscrapers and the like are lined up, and various radio waves travel over the ground, so that there is a risk that the ship may be temporarily unmaneuverable due to radio interference or radio interference, or may contact ground structures. Therefore, the present invention has been made in view of the drawbacks of the prior art,
It is an object of the present invention to provide an automatic ship maneuvering device for an airship that does not require operator training and can safely fly even if there is interference or radio interference.

【0004】[0004]

【課題を解決するための手段】すなわち本発明は、コン
ピュータに入力された航法プログラムに基づき自動航行
するように構成された飛行船において、該飛行船の船体
の上下、前後、左右に装着され常時超音波を発信すると
共に障害物からの反射音波を受信する超音波センサー及
び距離測定回路とからなる検知装置と、該検知装置から
の検知信号に基づき操作部に対して回避行動を指示する
制御装置とからなり、前記検知装置が障害物から所定距
離内に飛行船が近づいた時に制御装置に対して検知信号
を発信するように構成された飛行船の障害物自動回避装
置付自動操船装置により本目的を達成する。
That is, the present invention relates to an airship configured to automatically navigate based on a navigation program input to a computer, and is installed on the hull of the airship up, down, front and back, left and right, and is always subjected to ultrasonic waves. From a detection device including an ultrasonic sensor that transmits a sound and a reflected sound wave from an obstacle and a distance measurement circuit, and a control device that instructs the operation unit to perform an avoidance action based on a detection signal from the detection device. The above object is achieved by an automatic ship maneuvering device with an automatic obstacle avoidance device for an airship, wherein the detection device is configured to send a detection signal to a control device when the airship approaches within a predetermined distance from an obstacle. .

【0005】[0005]

【作用】すなわち、飛行船の前後左右及び上下に障害物
が存在しない時には制御装置は予めコンピュータに入力
された航法プログラムに従い制御装置が操船を行う。飛
行船の進路付近(前後左右上下)に障害物が存在する場
合には、飛行船の前後左右上下の6ヵ所に設けた検知装
置により障害物が所定の距離(危険距離)内にあるかど
うかが検知され、その結果所定距離内に障害物が存在す
る時には、検知装置から制御装置に対して検知信号が発
信され、その検知信号に基づき制御装置が操作部を操作
して、航法プログラムに優先して障害物の位置にあわせ
て左右、上下等に回避させるようにしている。その結
果、飛行船は無人飛行ながらオペレータなしで障害物を
回避しながら安全に飛行することができると共に電波障
害があっても安全に航行することができる。
That is, when there are no obstacles on the front, rear, left, right, and top and bottom of the airship, the control unit operates the ship in accordance with the navigation program previously input to the computer. If there are obstacles near the path of the airship (front, back, left, right, top and bottom), the detection devices provided at the 6 front, back, left, right, top and bottom of the airship will detect if the obstacle is within a predetermined distance (dangerous distance). As a result, when there is an obstacle within the predetermined distance, the detection device sends a detection signal to the control device, and the control device operates the operation unit based on the detection signal to give priority to the navigation program. The left and right, up and down, etc. are avoided according to the position of the obstacle. As a result, the airship can fly safely while avoiding obstacles without an operator while flying unmanned, and can navigate safely even if there is a radio interference.

【0006】[0006]

【実施例】以下に本発明を図示した実施例に従って詳細
に説明する。無人飛行船としては、屋内座標をチェック
しながら航行させるもの(屋内座標系)、地球座標をチ
ェックしながら航行させるもの(地球座標系)、予めラ
ジコン等でデモ飛行させ速度、舵角度及び時間等を記憶
させておきその記憶に基づき航行させるもの(デモ飛行
系)、地上からラジコン等で飛行船の操作部を操作して
航行させるもの(ラジコン系)等がある。屋内座標系
は、地上にビーコン発信器1個以上を3次元的に設置
し、該ビーコン発信器からの電波を受信して空間座標及
び傾きを求めながら航行するタイプのもので、主に屋内
空間を航行させるのに用いる。地球座標系は、飛行船に
GPS(グローバル・ポジショニング・システム)受信
機から得られる平面座標、高度及び傾き等に基づいて飛
行コースを修正しながら航行させるもので、屋外航行に
適する。
The present invention will be described in detail below with reference to the illustrated embodiments. As an unmanned airship, one that allows navigation while checking indoor coordinates (indoor coordinate system), one that allows navigation while checking earth coordinates (earth coordinate system), and make a demonstration flight with a radio control etc. in advance, speed, rudder angle, time, etc. There are things that are stored in memory and navigate based on that memory (demo system), and those that operate by manipulating the operating unit of an airship such as a radio-controlled model from the ground (radio system). The indoor coordinate system is a type in which one or more beacon transmitters are three-dimensionally installed on the ground, and the radio waves from the beacon transmitters are received to obtain spatial coordinates and inclination while navigating. Used to navigate. The earth coordinate system allows an airship to navigate while correcting the flight course based on plane coordinates, altitude, and tilt obtained from a GPS (Global Positioning System) receiver, and is suitable for outdoor navigation.

【0007】以下の実施例では地球座標系の飛行船の場
合に関して説明する。図に示すものは一般的な飛行船で
あり、飛行船1の前部、後部、左中腹部、右中腹部、上
部及び下部にそれぞれ(好ましくは30°乃至90°)
指向性を有し超音波を発信・受信する超音波センサー2
a,3a,4a,5a,6a,7aと、該超音波センサ
ーの発信から受信までの時間より障害物までの距離を算
出する距離測定回路2b,3b,4b,5b,6b,7
bとからなる検知装置が装着されており、該検知装置か
らの検知結果は制御装置8に検知信号(検知距離x1
x2,x3,x4,x5,x6)として入力される。尚、超音波セ
ンサーの指向性を90°に設定した時には、各超音波セン
サーにおける計測地点が異なるために超音波センサーの
検知方向が平行となり同じ物体に対して同時に反応する
ことはない
In the following embodiment, the case of an airship in the earth coordinate system will be described. What is shown in the figure is a general airship, and the airship 1 has a front part, a rear part, a left abdomen, a right abdomen, an upper part and a lower part (preferably 30 ° to 90 °).
Ultrasonic sensor 2 that has directivity and transmits and receives ultrasonic waves
a, 3a, 4a, 5a, 6a, 7a and distance measuring circuits 2b, 3b, 4b, 5b, 6b, 7 for calculating the distance to the obstacle from the time from the transmission to the reception of the ultrasonic sensor
b is attached, and the detection result from the detection device is sent to the control device 8 as a detection signal (detection distance x 1 ,
x 2 , x 3 , x 4 , x 5 , x 6 ) are input. In addition, when the directivity of the ultrasonic sensor is set to 90 °, the detection points of the ultrasonic sensors are parallel because the measurement points in each ultrasonic sensor are different and do not react to the same object at the same time.

【0008】この制御装置8には、予めその記憶装置に
飛行船から障害物までの危険距離d1,d2,d3,d4,d5
d6が入力されており、該危険距離d1,d2,d3,d4,d5
d6と検知距離x1,x2,x3,x4,x5,x6とが比較回路で比
較され、さらに比較結果が回避方向判断回路に入力さ
れ、該回避方向判断回路が表1に示すように判断し、C
PUに対して自動操船に優先するよう信号を出して入力
方法を切り替えさせると共に推進機9と舵10からなる操
作部Aを操作して回避行動をとらせる。この危険距離
d1,d2,d3,d4,d5,d6は、別に同じ距離に設定する必
要はなくd1を一番長めに設定するのが一般的である。
尚、本実施例における表に示す制御では、6個設けた超
音波センサーの内の最高2つの超音波センサーが検知す
る順列組合せの場合について示したが、これに限定され
るものではなく、それぞれのセンサーが2通りの検知
(危険・安全)を行うと考えると単純に26(64)通り
の制御の仕方があり、これらを予め制御装置8に入力し
ておいても良い。実際には、無限通りの制御方式があ
り、使用方法により適宜選択する。
The control device 8 has previously stored in its storage device dangerous distances d 1 , d 2 , d 3 , d 4 , d 5 , from the airship to obstacles.
d 6 has been entered, and the dangerous distances d 1 , d 2 , d 3 , d 4 , d 5 ,
d 6 and the detection distances x 1 , x 2 , x 3 , x 4 , x 5 , x 6 are compared by a comparison circuit, and the comparison result is input to the avoidance direction determination circuit. And judge as shown in
A signal is issued to the PU so as to give priority to automatic marine vessel maneuvering, and the input method is switched. At the same time, the operating section A composed of the propulsion unit 9 and the rudder 10 is operated to take an avoidance action. This dangerous distance
d 1, d 2, d 3 , d 4, d 5, d 6 are separately common to set requires d 1, not most longer be set to the same distance.
In the control shown in the table in the present embodiment, the case of the permutation combination detected by up to two ultrasonic sensors among the six ultrasonic sensors provided has been described, but the present invention is not limited to this, and There are two types of sensors
Considering that (danger / safety) is performed, there are simply 2 6 (64) ways of control, and these may be input to the control device 8 in advance. Actually, there are an infinite number of control methods, and the control method is appropriately selected according to the usage method.

【0009】[0009]

【表1】 [Table 1]

【0010】また制御装置8には、その内部コンピュー
タ(CPU)に予め飛行船の飛行経路及び飛行方法等の
プログラム(座標・時間等)が入力されており、該制御
装置8は飛行船1内に装着されたGPS受信機12用の4
つ以上のGPS衛星から発信された電波の受信データの
解析結果に基づき飛行船の経度、緯度、高度及び3軸の
姿勢をプログラムされたデータと比較し、操作部Aを操
作して位置及び姿勢を制御しながら飛行するように構成
されており、さらに算出される飛行速度に基づき推進機
9の出力の増減も行うように構成されている。尚、本実
施例の制御装置8では、航法プログラムに基づく自動航
行中に各検知装置からの検知信号を受信した時には、衝
突防止の観点から操作部Aに航法プログラムに優先する
べく入力切替回路が回避方向判断回路からの指示に従い
回避行動をとるように構成されている。また本実施例に
かかる制御装置8には、ラジコン受信機16が装着されて
おり、制御装置8に対して無線方式で飛行経路の変更及
び推進機9並びに舵10の操船を指示できるように構成さ
れている。尚、14は、GPS受信機12で算出される高度
とを比較するための既知の高度計であり、19はGPS受
信機12で算出される姿勢と比較するための既知の3軸ジ
ャイロセンサーである。
A program (coordinates, time, etc.) such as the flight route and flight method of the airship is input to the internal computer (CPU) of the control device 8 in advance, and the control device 8 is installed in the airship 1. 4 for GPS receiver 12
Compare the longitude, latitude, altitude, and 3-axis attitude of the airship with the programmed data based on the analysis results of the received data of the radio waves transmitted from one or more GPS satellites, and operate the operation unit A to determine the position and attitude. It is configured to fly under control, and is further configured to increase or decrease the output of the propulsion unit 9 based on the calculated flight speed. In the control device 8 of the present embodiment, when a detection signal is received from each detection device during automatic navigation based on the navigation program, the operation unit A has an input switching circuit to prioritize the navigation program from the viewpoint of collision prevention. It is configured to take avoidance action according to an instruction from the avoidance direction determination circuit. Further, the control device 8 according to the present embodiment is equipped with a radio control receiver 16 and is configured to be able to instruct the control device 8 to change the flight path and maneuver the propulsion device 9 and the rudder 10 in a wireless manner. Has been done. Incidentally, 14 is a known altimeter for comparing with the altitude calculated by the GPS receiver 12, and 19 is a known three-axis gyro sensor for comparing with the attitude calculated by the GPS receiver 12. .

【0011】さらに、飛行経路の位置確認のための精度
を上げるためには、経度、緯度及び高度が別の手段によ
り測定されている地上の基準点に別個にGPS受信機12
aを設置し、該GPS受信機12aが解析する経度、緯
度、高度及び電波のキャリアと基準点の座標とを比較し
てそれぞれの測定データの補正値を算出し、さらにそれ
ら補正値等を送信機を介して飛行船1の受信機18に送信
し、該受信機18からCPUに入力することにより飛行船
1のGPS受信機12で解析した測定値を補正するように
すれば良い。
Further, in order to improve the accuracy for confirming the position of the flight route, the GPS receiver 12 is separately provided at the ground reference point whose longitude, latitude and altitude are measured by other means.
a is installed, the longitude, latitude, altitude, and the carrier of radio waves analyzed by the GPS receiver 12a are compared with the coordinates of the reference point to calculate the correction values of the respective measurement data, and the correction values are transmitted. The measurement value analyzed by the GPS receiver 12 of the airship 1 may be corrected by transmitting the data to the receiver 18 of the airship 1 via the aircraft and inputting it to the CPU from the receiver 18.

【0012】尚、制御装置8の内部コンピュータに基づ
く自動航行に関して、GPS受信機12を用いた方式につ
いて述べたがこれに限定されるものではなく、オペレー
タが最初に無線誘導で所定の飛行経路をデモ飛行させる
と共にその際に舵の角度及び時間、推進機の回転数等を
記憶装置に記憶させておき、2回目以降の飛行に際して
は予め記憶装置に記憶させたデータに基づき操船装置を
作動させ自動航行するようにしたデモ飛行系や、屋内座
標系の自動航行システムに採用しても良い。本実施例で
は飛行船の前方に障害物が存在した時に右へ旋回させる
ように構成したがこれに限定されるものではなく、左方
向へ旋回させるように構成してもよく、旋回角度として
は進行方向に対して20°程度にするのが望ましい。ま
た検知装置による検知信号が2つ重なった時(例えば左
右、上下)に停止させるように構成したが、これに限定
されるものではなく一旦停止させた後に後進させ、上下
又は左右方向に方向転換させるように構成しても良い。
The automatic navigation based on the internal computer of the control unit 8 has been described with respect to the system using the GPS receiver 12, but the system is not limited to this. The operator first makes a predetermined flight route by wireless guidance. At the same time as making a demonstration flight, the angle and time of the rudder, the number of revolutions of the propulsion unit, etc. were stored in the storage device, and during the second and subsequent flights, the boat maneuvering device was operated based on the data stored in advance in the storage device. It may be used for a demo flight system that is designed to automatically navigate and an automatic navigation system for indoor coordinate systems. In the present embodiment, it is configured to turn to the right when there is an obstacle in front of the airship, but the present invention is not limited to this, and it may be configured to turn to the left, and as a turning angle, It is desirable that the angle is about 20 ° with respect to the direction. Further, although it is configured to stop when two detection signals from the detection device are overlapped (for example, left and right, up and down), the invention is not limited to this, and after stopping once, the vehicle is moved backward and the direction is changed vertically or horizontally. You may comprise so that it may be made.

【0013】以上述べた構成において本実施例にかかる
装置では予め航法プログラムに図3に示すような飛行船
1が通過すべきポイントP1,P2,P3,P4(経度、緯度、
高度、速度等)を制御装置8の記憶装置に記憶してお
く。すると飛行船1は障害物が存在しない状態において
は各ポイントを目指し、GPS受信機12で経度、緯度、
高度及び速度並びに3軸の傾きを算出し、航法データと
比較しながら制御装置8が推進機9及び舵10等の操作部
Aを操作しながら航行させる。そして進行方向に障害物
が存在した場合には、航法プログラムに優先するように
切替え、検知装置からの検知信号に基づき回避方向判断
回路が表1に示すように操作部Aを操作して飛行船を上
下左右方向に方向転換して回避し、検知装置からの検知
危険信号がなくなった時点(危険距離d1,d2,d3,d4
d5,d6より検知距離x1,x2,x3,x4,x5,x6のいずれも
が長くなったとき)で、再度航法プログラムに基づいた
自動操船に切り替える。そして一旦各ポイントを通過し
た後には、次のポイントを目指して操船させることにな
る。
In the apparatus according to the present embodiment having the above-described configuration, points P 1 , P 2 , P 3 , P 4 (longitude, latitude,
The altitude, speed, etc.) are stored in the storage device of the control device 8. Then, the airship 1 aims at each point when there are no obstacles, and the GPS receiver 12 uses the longitude, latitude,
The control device 8 operates the operation unit A such as the propulsion unit 9 and the rudder 10 while the altitude and speed and the inclination of the three axes are calculated, and compares the navigation data with the navigation data. When there is an obstacle in the traveling direction, the navigation program is switched to be prioritized, and the avoidance direction determination circuit operates the operation unit A as shown in Table 1 based on the detection signal from the detection device to operate the airship. At the time when there is no detection danger signal from the detection device (direction of danger distance d 1 , d 2 , d 3 , d 4 ,
When any of the detection distances x 1 , x 2 , x 3 , x 4 , x 5 , x 6 becomes longer than d 5 , d 6 ), switch to automatic navigation based on the navigation program again. Then, after passing through each point, the maneuvering will be aimed at the next point.

【0014】[0014]

【効果】以上述べたように本発明にかかる装置では、無
線操縦によらず、予めコンピュータに記憶された飛行経
路に沿って飛行船を航行させることができると共に、そ
の航路上に障害物が存在した場合に自動航法プログラム
に優先して飛行船の前後左右上下の各場所に設置した検
知装置からの検知信号に基づき障害物を自動的に回避す
るように構成されていることから、無線操縦のオペレー
タの育成が不要になると共にオペレータには操作ではな
く監視させるだけで済むので、長時間の飛行が行え、そ
の利用価値は従来の装置に比較して大きい。
As described above, in the device according to the present invention, an airship can be made to travel along a flight route stored in a computer in advance without any radio control, and an obstacle exists on the route. In this case, since it is configured to automatically avoid obstacles based on the detection signals from the detection devices installed at the front, rear, left, right, top and bottom of the airship in preference to the automatic navigation program, Since the training is not necessary and the operator only needs to monitor the operation, not the operation, the flight can be performed for a long time, and its utility value is greater than that of the conventional apparatus.

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

【図1】 本発明にかかる装置を搭載した飛行船の側面
図である。
FIG. 1 is a side view of an airship equipped with a device according to the present invention.

【図2】 本発明にかかる装置のブロック図である。FIG. 2 is a block diagram of an apparatus according to the present invention.

【図3】 本発明にかかる操船装置を搭載した飛行船に
飛行経路と障害物回避した場合の飛行経路を示す航跡図
である。
FIG. 3 is a track diagram showing a flight path and a flight path when an obstacle is avoided in an airship equipped with the ship manipulating apparatus according to the present invention.

【図4】 本発明にかかる装置の地球座標系における作
動を示すフローチャートである。
FIG. 4 is a flowchart showing the operation of the device according to the present invention in the earth coordinate system.

【符号の説明】[Explanation of symbols]

1 飛行船 2a,3a,4a,5a,6a,7a 超音波センサー 2b,3b,4b,5b,6b,7b 距離測定回路 8 制御装置 9 推進機 10 舵 12 GPS受信機 14 高度計 16 ラジコン受信機 18 受信機 19 ジャイロセンサー 1 Airship 2a, 3a, 4a, 5a, 6a, 7a Ultrasonic sensor 2b, 3b, 4b, 5b, 6b, 7b Distance measuring circuit 8 Control device 9 Propulsion device 10 Rudder 12 GPS receiver 14 Altimeter 16 Radio control receiver 18 Reception Machine 19 gyro sensor

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 コンピュータに入力された航法プログラ
ムに基づき自動航行するように構成された飛行船におい
て、該飛行船の船体の上下、前後、左右に装着され常時
音波を発信すると共に障害物からの反射音波を受信する
超音波センサー及び距離測定回路とからなる検知装置
と、該検知装置からの検知信号に基づき操作部に対して
回避行動を指示する制御装置とからなり、前記検知装置
が障害物から所定距離内に飛行船が近づいた時に制御装
置に対して検知信号を発信するように構成された飛行船
の障害物自動回避装置付自動操船装置。
1. An airship configured to automatically navigate based on a navigation program input to a computer. The airship is attached to the top, bottom, front, back, left and right of the hull of the airship to constantly emit sound waves and reflected sound waves from obstacles. A detection device including an ultrasonic sensor and a distance measuring circuit for receiving the information, and a control device for instructing the operation unit to perform an avoidance action based on a detection signal from the detection device. An automatic vessel maneuvering device with an automatic obstacle avoidance device for an airship, which is configured to send a detection signal to a control device when the airship approaches within a distance.
【請求項2】 制御装置が、航法プログラムに基づく操
船に優先して回避行動を操作部に採らせ、検知信号がな
くなった時には再びプログラム制御の操船に切り替える
ものである請求項1記載の飛行船の障害物自動回避装置
付自動操船装置。
2. The airship according to claim 1, wherein the control device causes the operation section to take the avoidance action in preference to the marine vessel maneuvering based on the navigation program, and switches to the program controlled marine vessel maneuver again when the detection signal disappears. Automatic ship handling system with automatic obstacle avoidance system.
JP5658593A 1993-02-22 1993-02-22 Automatic airship control device with automated obstacle avoidance device Pending JPH06247393A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5658593A JPH06247393A (en) 1993-02-22 1993-02-22 Automatic airship control device with automated obstacle avoidance device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5658593A JPH06247393A (en) 1993-02-22 1993-02-22 Automatic airship control device with automated obstacle avoidance device

Publications (1)

Publication Number Publication Date
JPH06247393A true JPH06247393A (en) 1994-09-06

Family

ID=13031261

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5658593A Pending JPH06247393A (en) 1993-02-22 1993-02-22 Automatic airship control device with automated obstacle avoidance device

Country Status (1)

Country Link
JP (1) JPH06247393A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0725392A (en) * 1993-07-14 1995-01-27 Japan Aviation Electron Ind Ltd Remote control type airframe system for unmanned flying body
US6857601B2 (en) 2001-07-06 2005-02-22 Seiko Epson Corporation Airship system
KR100472968B1 (en) * 2002-11-04 2005-03-08 한국항공우주연구원 Autonomous Take-Off and Landing System for Large-Class Unmanned Airship
CN106662879A (en) * 2014-06-25 2017-05-10 亚马逊科技公司 Object avoidance for automated aerial vehicles
JP2018199915A (en) * 2017-05-26 2018-12-20 西松建設株式会社 Aqueduct tunnel inspection apparatus and system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0725392A (en) * 1993-07-14 1995-01-27 Japan Aviation Electron Ind Ltd Remote control type airframe system for unmanned flying body
US6857601B2 (en) 2001-07-06 2005-02-22 Seiko Epson Corporation Airship system
US6908061B2 (en) 2001-07-06 2005-06-21 Seiko Epson Corporation Airship system
KR100472968B1 (en) * 2002-11-04 2005-03-08 한국항공우주연구원 Autonomous Take-Off and Landing System for Large-Class Unmanned Airship
CN106662879A (en) * 2014-06-25 2017-05-10 亚马逊科技公司 Object avoidance for automated aerial vehicles
JP2017519297A (en) * 2014-06-25 2017-07-13 アマゾン テクノロジーズ インコーポレイテッド Object avoidance for automated aircraft
US10762797B2 (en) 2014-06-25 2020-09-01 Amazon Technologies, Inc. Object avoidance methods for automated aerial vehicles
JP2018199915A (en) * 2017-05-26 2018-12-20 西松建設株式会社 Aqueduct tunnel inspection apparatus and system

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