UNMANNED AIRCRAFT CONTROL SYSTEM

• Main Authors: YUASA TAKAYUKI, IMANAKA MASAYUKI, YAMADA HIROHISA, ISHIMARU KENGO, OSAWA JUNJI
• Format: Patent
• Language: English; Japanese
• Published: 28.01.2021
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; CONTROLLING; COSMONAUTICS; ELECTRIC COMMUNICATION TECHNIQUE; ELECTRICITY; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; PHYSICS; PICTORIAL COMMUNICATION, e.g. TELEVISION; REGULATING; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES; TRANSPORTING

To provide an unmanned aircraft control system capable of improving operability so as to prevent an unmanned aircraft from approaching an obstacle or the like or entering a flying inhibited region.SOLUTION: This unmanned aircraft control system comprises: an unmanned aircraft 10 that has a first azimuth sensor 19 for detecting a front azimuth; and a portable terminal 50 that has a control unit 59 for controlling flying of the unmanned aircraft 10. The control unit 59 comprises an azimuth setting unit 59c for setting a target azimuth, a turning angle calculation unit 59d that calculates the turning angle of the unmanned aircraft 10, and an azimuth control unit 59e that turns the unmanned aircraft 10 on the basis of the turning angle, and changes the front azimuth of the unmanned aircraft 10 to the target azimuth.SELECTED DRAWING: Figure 5 【課題】無人航空機による障害物等への接近や飛行禁止区域への侵入を回避可能に、操縦性を向上させることが可能な無人航空機制御システムを提供する。【解決手段】無人航空機制御システムは、前方の方位を検出する第１方位センサ１９を有する無人航空機１０と、無人航空機１０の飛行を制御する制御部５９を有する携帯端末５０と、を備え、制御部５９は、目標方位を設定する方位設定部５９ｃと、無人航空機１０の旋回角度を算出する旋回角度算出部５９ｄと、旋回角度に基づいて無人航空機１０を旋回させ無人航空機１０の前方の方位を目標方位に変更する方位制御部５９ｅと、を備える。【選択図】図５