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Publication number
JP2019197475A5
JP2019197475A5 JP2018092203A JP2018092203A JP2019197475A5 JP 2019197475 A5 JP2019197475 A5 JP 2019197475A5 JP 2018092203 A JP2018092203 A JP 2018092203A JP 2018092203 A JP2018092203 A JP 2018092203A JP 2019197475 A5 JP2019197475 A5 JP 2019197475A5
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JP
Japan
Prior art keywords
flight
unit
lost
flight device
surveying
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
JP2018092203A
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Japanese (ja)
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JP2019197475A (en
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Publication date
Application filed filed Critical
Priority to JP2018092203A priority Critical patent/JP2019197475A/en
Priority claimed from JP2018092203A external-priority patent/JP2019197475A/en
Priority to PCT/JP2019/014969 priority patent/WO2019194277A1/en
Publication of JP2019197475A publication Critical patent/JP2019197475A/en
Publication of JP2019197475A5 publication Critical patent/JP2019197475A5/ja
Priority to US17/060,414 priority patent/US20210026375A1/en
Pending legal-status Critical Current

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Claims (5)

光を照射元へ反射する再帰反射部材(15)を有する飛行装置(11)と、
前記飛行装置(11)へ光を照射するとともに、前記再帰反射部材(15)で反射した光から、前記飛行装置(11)を追尾して、前記飛行装置(11)までの距離および前記飛行装置(11)の飛行角度を飛行データとして取得する測量部(12)と、
前記測量部(12)で取得した飛行データに基づいて、前記飛行装置(11)の飛行を制御する地上基地(13)と、を備える飛行装置誘導システムにおいて、
前記測量部(12)で取得した飛行データのみに基づいて、前記飛行装置(11)の飛行中に、前記測量部(12)が前記再帰反射部材(15)の追尾を維持しているか否かを判定する追尾判定部(71)と、
前記追尾判定部(71)において前記再帰反射部材(15)の追尾が維持されていないロスト判定がされたとき、前記ロスト判定がなされた前記飛行装置(11)の飛行位置をロスト位置と定義するロスト位置定義部(72)と、
前記ロスト判定がされたとき、前記測量部(12)を駆動して、前記ロスト位置を中心に前記再帰反射部材(15)を探索する探索制御部(73)と、
前記ロスト判定がされたとき、前記飛行装置(11)の飛行にともなう移動を停止し、前記飛行装置(11)をその場に停止する制御を行なう停止制御部(74)と、
を備える飛行装置誘導システム。
A flight device (11) having a retroreflective member (15) for reflecting light to an irradiation source;
The flight device (11) is irradiated with light, and the flight device (11) is tracked from the light reflected by the retroreflective member (15) to determine the distance to the flight device (11) and the flight device. A surveying section (12) for acquiring the flight angle of (11) as flight data;
A flight device guidance system comprising: a ground base (13) for controlling flight of the flight device (11) based on flight data acquired by the surveying unit (12),
Whether the surveying unit (12) maintains tracking of the retroreflective member (15) during flight of the flight device (11) based on only the flight data acquired by the surveying unit (12). A tracking determination unit (71) for determining
When the tracking determination unit (71) makes a lost determination that tracking of the retroreflective member (15) is not maintained, the flight position of the flight device (11) that has made the lost determination is defined as a lost position. A lost position definition unit (72),
A search control unit (73) that drives the surveying unit (12) to search for the retroreflective member (15) around the lost position when the lost determination is made,
A stop control unit (74) for controlling, when the lost determination is made, stopping movement of the flying device (11) during flight and stopping the flying device (11) in place;
A flight device guidance system.
光を照射元へ反射する再帰反射部材(15)を有する飛行装置(11)と、
前記飛行装置(11)へ光を照射するとともに、前記再帰反射部材(15)で反射した光から、前記飛行装置(11)を追尾して、前記飛行装置(11)までの距離および前記飛行装置(11)の飛行角度を飛行データとして取得する測量部(12)と、
前記測量部(12)で取得した飛行データに基づいて、前記飛行装置(11)の飛行を制御する地上基地(13)と、を備える飛行装置誘導システムにおいて、
前記測量部(12)で取得した飛行データのみに基づいて、前記飛行装置(11)の飛行中に、前記測量部(12)が前記再帰反射部材(15)の追尾を維持しているか否かを判定する追尾判定部(71)と、
前記追尾判定部(71)において前記再帰反射部材(15)の追尾が維持されていないロスト判定がされたとき、前記ロスト判定がなされた位置をロスト位置と定義するロスト位置定義部(72)と、
前記ロスト判定がされたとき、前記測量部(12)を駆動して、前記ロスト位置を中心に前記再帰反射部材(15)を探索する探索制御部(73)と、
前記ロスト判定がされたとき、前記飛行装置(11)の飛行にともなう移動を停止し、前記ロスト判定がされた前記飛行装置(11)を、前記ロスト位置に戻して停止する制御を行なう停止制御部(74)と、
を備える飛行装置誘導システム。
A flight device (11) having a retroreflective member (15) for reflecting light to an irradiation source;
The flight device (11) is irradiated with light, and the flight device (11) is tracked from the light reflected by the retroreflective member (15) to determine the distance to the flight device (11) and the flight device. A surveying section (12) for acquiring the flight angle of (11) as flight data;
A flight device guidance system comprising: a ground base (13) for controlling flight of the flight device (11) based on flight data acquired by the surveying unit (12),
Whether the surveying unit (12) maintains tracking of the retroreflective member (15) during the flight of the flying device (11) based on only the flight data acquired by the surveying unit (12). A tracking determination unit (71) for determining
When the tracking determination unit (71) makes a lost determination that tracking of the retroreflective member (15) is not maintained, a lost position defining unit (72) that defines the position where the lost determination is made as a lost position. ,
A search control unit (73) that drives the surveying unit (12) to search for the retroreflective member (15) around the lost position when the lost determination is made,
When the lost determination is made, stop control for stopping the movement of the flying device (11) accompanying flight and returning the flying device (11) for which the lost determination is made to the lost position and stopping. Part (74),
A flight guidance system.
前記飛行装置(11)に設けられ、自身の飛行位置を自立的に取得する位置取得部(34)と、
前記飛行装置(11)に設けられ、前記ロスト判定がされたとき、前記位置取得部(34)で取得した前記飛行位置に基づいて飛行を制御する位置制御部(35)と、
をさらに備える請求項1または2記載の飛行装置誘導システム。
A position acquisition unit (34) provided in the flight device (11) and autonomously acquiring its own flight position;
A position control unit (35) provided in the flight device (11), which controls flight based on the flight position acquired by the position acquisition unit (34) when the lost determination is made;
The flight device guidance system according to claim 1, further comprising:
光を照射元へ反射する再帰反射部材(15)を有する飛行装置(11)と、
前記飛行装置(11)へ光を照射するとともに、前記再帰反射部材(15)で反射した光から、前記飛行装置(11)を追尾して、前記飛行装置(11)までの距離および前記飛行装置(11)の飛行角度を飛行データとして取得する測量部(12)と、
前記測量部(12)で取得した飛行データに基づいて、前記飛行装置(11)の飛行を制御する地上基地(13)と、を備える飛行装置誘導システムにおいて、
前記飛行装置(11)に設けられ、自身の飛行位置を自立的に取得する位置取得部(34)と、
前記測量部(12)で取得した飛行データのみに基づいて、前記飛行装置(11)の飛行中に、前記測量部(12)が前記再帰反射部材(15)の追尾を維持しているか否かを判定する追尾判定部(71)と、
前記追尾判定部(71)において前記再帰反射部材(15)の追尾が維持されていないロスト判定がされたとき、前記位置取得部(34)で取得した前記飛行位置を前記測量部(12)へ伝達する通信部(31)と、
前記測量部(12)を駆動して、前記通信部(31)を通して前記測量部(12)へ伝達された前記飛行位置を中心に前記再帰反射部材(15)を探索する探索制御部(73)と、
を備える飛行装置誘導システム。
A flight device (11) having a retroreflective member (15) for reflecting light to an irradiation source;
The flight device (11) is irradiated with light, and the flight device (11) is tracked from the light reflected by the retroreflective member (15) to determine the distance to the flight device (11) and the flight device. A surveying section (12) for acquiring the flight angle of (11) as flight data;
A flight device guidance system comprising: a ground base (13) for controlling flight of the flight device (11) based on flight data acquired by the surveying unit (12),
A position acquisition unit (34) provided in the flight device (11) and autonomously acquiring its own flight position;
Whether the surveying unit (12) maintains tracking of the retroreflective member (15) during flight of the flight device (11) based on only the flight data acquired by the surveying unit (12). A tracking determination unit (71) for determining
When the tracking determination unit (71) makes a lost determination that the tracking of the retroreflective member (15) is not maintained, the flight position acquired by the position acquisition unit (34) is sent to the surveying unit (12). A communication unit (31) for transmitting,
A search control unit (73) that drives the surveying unit (12) to search for the retroreflective member (15) around the flight position transmitted to the surveying unit (12) through the communication unit (31). When,
A flight device guidance system.
前記飛行装置(11)に設けられ、前記ロスト判定がされたとき、前記位置取得部(34)で取得した前記飛行位置に基づいて、前記飛行装置(11)の飛行を継続する飛行制御部(35)をさらに備える請求項4記載の飛行装置誘導システム。 A flight control unit that is provided in the flight device (11) and continues the flight of the flight device (11) based on the flight position acquired by the position acquisition unit (34) when the lost determination is made. 35. The flight device guidance system of claim 4, further comprising: 35).
JP2018092203A 2018-04-05 2018-05-11 Flight device guide system Pending JP2019197475A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP2018092203A JP2019197475A (en) 2018-05-11 2018-05-11 Flight device guide system
PCT/JP2019/014969 WO2019194277A1 (en) 2018-04-05 2019-04-04 Flying device and flying device guidance system
US17/060,414 US20210026375A1 (en) 2018-04-05 2020-10-01 Aircraft and aircraft guidance system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2018092203A JP2019197475A (en) 2018-05-11 2018-05-11 Flight device guide system

Publications (2)

Publication Number Publication Date
JP2019197475A JP2019197475A (en) 2019-11-14
JP2019197475A5 true JP2019197475A5 (en) 2020-07-30

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JP2018092203A Pending JP2019197475A (en) 2018-04-05 2018-05-11 Flight device guide system

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7226586B2 (en) 2019-11-20 2023-02-21 日本電気株式会社 Mobile body control system, mobile body control device, and mobile body control method
JP7421396B2 (en) 2020-03-27 2024-01-24 株式会社Nttデータ Autonomous flying vehicle and flight control method

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2022185210A (en) * 2021-06-02 2022-12-14 空撮サービス株式会社 Unmanned aerial vehicle position measurement system, and position measurement method

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006284385A (en) * 2005-03-31 2006-10-19 Nec Toshiba Space Systems Ltd GPS satellite reference station system
JP6693765B2 (en) * 2016-02-26 2020-05-13 株式会社トプコン Flight object tracking method and flight object guidance system
JP2017173254A (en) * 2016-03-25 2017-09-28 東京電力ホールディングス株式会社 Radiation dosimetry device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7226586B2 (en) 2019-11-20 2023-02-21 日本電気株式会社 Mobile body control system, mobile body control device, and mobile body control method
JP7421396B2 (en) 2020-03-27 2024-01-24 株式会社Nttデータ Autonomous flying vehicle and flight control method

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