MA41572B1 - Autonomous navigation and behavior of unmanned vehicle without connection to the control station - Google Patents
Autonomous navigation and behavior of unmanned vehicle without connection to the control stationInfo
- Publication number
- MA41572B1 MA41572B1 MA41572A MA41572A MA41572B1 MA 41572 B1 MA41572 B1 MA 41572B1 MA 41572 A MA41572 A MA 41572A MA 41572 A MA41572 A MA 41572A MA 41572 B1 MA41572 B1 MA 41572B1
- Authority
- MA
- Morocco
- Prior art keywords
- mission
- connection
- behavior
- decision
- control station
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0088—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot characterized by the autonomous decision making process, e.g. artificial intelligence, predefined behaviours
Abstract
Les systèmes de dècision autonomes qui sont utilisés dans les avions sans pilotes sont conçus pour gérer des imprévus tels que la perte de connexion. Dans un tel cas, selon l'implémentation du système, celui-ci exécute un retour à la base en essayant de minimiser les risques, sinon, il veille à continuer l'exécution de la mission avec un mécanisme de cycles d'évaluations et de corrections le temps que la connexion soit rétablie. Ces implémentations, par leurs conceptions, permettent au système de fonctionner avec des performances définies par défaut sans qu'ils ne soient capables de prendre des initiatives, changer de mission en vol, gérer les situations d'incertitude, ni être totalement indépendants d'une station de contrôle. Nous proposons un système et méthode avec une conception où le fonctionnement en autonomie décisionnelle est le moyen principal d'opérer l'avion sans pilote pendant toute la mission, incluant le décollage et l'atterrissage. La commande à distance depuis une station au sol est secondaire. Cette autonomie décisionnelle est implémentée par trois modules de comportement, de vision et de mission dont l'implémentation et le fonctionnement sont décrit dans ce document.Autonomous decision systems that are used in unmanned aircraft are designed to deal with unforeseen events such as loss of connection. In such a case, depending on the implementation of the system, it performs a return to base trying to minimize the risks, otherwise, it ensures to continue the execution of the mission with a mechanism of cycles of evaluations and corrections while the connection is reestablished. These implementations, by their designs, allow the system to operate with performance defined by default without being able to take initiatives, change mission in flight, manage situations of uncertainty, or be completely independent of a control station. We propose a system and method with a design where decision-making autonomy is the primary means of operating the unmanned aircraft during the entire mission, including take-off and landing. Remote control from a ground station is secondary. This decision-making autonomy is implemented by three behavior, vision and mission modules, the implementation and operation of which are described in this document.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MA41572A MA41572B1 (en) | 2017-12-05 | 2017-12-05 | Autonomous navigation and behavior of unmanned vehicle without connection to the control station |
PCT/MA2018/050013 WO2019112407A1 (en) | 2017-12-05 | 2018-12-04 | Autonomous pilotless vehicle navigation and behaviour without connection to the control station |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
MA41572A MA41572B1 (en) | 2017-12-05 | 2017-12-05 | Autonomous navigation and behavior of unmanned vehicle without connection to the control station |
Publications (2)
Publication Number | Publication Date |
---|---|
MA41572A1 MA41572A1 (en) | 2019-06-28 |
MA41572B1 true MA41572B1 (en) | 2019-08-30 |
Family
ID=65019551
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MA41572A MA41572B1 (en) | 2017-12-05 | 2017-12-05 | Autonomous navigation and behavior of unmanned vehicle without connection to the control station |
Country Status (2)
Country | Link |
---|---|
MA (1) | MA41572B1 (en) |
WO (1) | WO2019112407A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111353606B (en) * | 2020-02-29 | 2022-05-03 | 中国电子科技集团公司第五十二研究所 | Deep reinforcement learning air combat game method and system based on fuzzy decision tree |
CN111914412B (en) * | 2020-07-21 | 2023-07-04 | 同济大学 | Automatic drivability limitation testing system and method based on error injector |
CN112099525B (en) * | 2020-08-31 | 2021-10-15 | 北京航空航天大学 | Spacecraft formation flight low communication maintaining cooperative control method |
CN113110114B (en) * | 2021-05-24 | 2023-07-14 | 北京润科通用技术有限公司 | Scheduling method and device for super-real-time joint simulation |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7512462B2 (en) | 2004-11-16 | 2009-03-31 | Northrop Grumman Corporation | Automatic contingency generator |
US8078319B2 (en) | 2005-02-16 | 2011-12-13 | Lockheed Martin Corporation | Hierarchical contingency management system for mission planners |
US9250630B2 (en) * | 2011-08-16 | 2016-02-02 | Unmanned Innovation, Inc. | Modular flight management system incorporating an autopilot |
US9547311B2 (en) * | 2012-03-22 | 2017-01-17 | Israel Aerospace Industries Ltd. | Planning and monitoring of autonomous-mission |
EP3008535B1 (en) * | 2014-09-05 | 2018-05-16 | SZ DJI Technology Co., Ltd. | Context-based flight mode selection |
US9715235B2 (en) | 2015-06-05 | 2017-07-25 | The Boeing Company | Autonomous unmanned aerial vehicle decision-making |
-
2017
- 2017-12-05 MA MA41572A patent/MA41572B1/en unknown
-
2018
- 2018-12-04 WO PCT/MA2018/050013 patent/WO2019112407A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2019112407A1 (en) | 2019-06-13 |
MA41572A1 (en) | 2019-06-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
MA41572B1 (en) | Autonomous navigation and behavior of unmanned vehicle without connection to the control station | |
US8321068B2 (en) | Method of plotting a portion of trajectory of an aircraft comprising a circular arc of constant radius | |
US8781654B2 (en) | Method and device for aiding the approach of an aircraft during an approach phase for the purpose of landing | |
US7089091B2 (en) | Method and device for revising a flight plan of an aircraft | |
US8521343B2 (en) | Method and system to autonomously direct aircraft to emergency-contingency landing sites using on-board sensors | |
US7269486B2 (en) | Method and device for automatically determining a capture trajectory of a flight trajectory for an aircraft, as well as a procedure and system for automatic guidance of an aircraft | |
US11676498B2 (en) | Enhanced vehicle efficiency through smart automation for on-board weather update | |
FR2905480A1 (en) | METHOD OF CHANGING THE ROAD FOLLOWED BY AN AIRCRAFT, THE AIRCRAFT ORIGINALLY FOLLOWING A PREDEFINED TRACK, THE METHOD FOR AN ANCILLARY RETURN OF THE AIRCRAFT ON THE PREDEFINED TRACK. | |
WO2013079666A1 (en) | Method for managing a vertical flight plan | |
CN111332483A (en) | System and method for providing flight path angle dependent thrust guidance | |
US10242578B2 (en) | Flight path management system | |
EP2525190A1 (en) | Device and method for building an air route to reach a destination | |
FR2926156A1 (en) | METHOD FOR TAKING INTO ACCOUNT A HTMB GUIDING INSTRUCTION. | |
FR2876789A1 (en) | METHOD FOR POSITIONING DIFFERENTLY EXECUTED ORDERS IN A FLIGHT TRACK OF AN AIRCRAFT | |
US20200103924A1 (en) | Systems and methods for optimized cruise vertical path | |
FR2954490A1 (en) | Method for dynamic management of flight procedure of flight plan of aircraft i.e. civil airplane, involves representing mandatory or optional flight characteristics of segment by additional attribute that is digitally coded in data base | |
EP3578925B1 (en) | Automatic from-waypoint updating system and method | |
FR3013466A1 (en) | METHOD FOR DETERMINING AN AIRCRAFT RESULTING TRACK, APPARATUS AND COMPUTER PROGRAM PRODUCT THEREOF | |
FR3043473A1 (en) | METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT FOR ENERGY MANAGEMENT DURING AN APPROACH PHASE. | |
FR3028498A1 (en) | DEVICE FOR CONTROLLING A PUSHING REGIME OF AT LEAST ONE AIRCRAFT ENGINE. | |
FR2924505A1 (en) | Side and vertical profile's automatic tracking modes decoupling method for e.g. civil aircraft, has disengaging automatic tracking mode of vertical profile automatically if separation criterion between aircraft and side profile is satisfied | |
US11417221B2 (en) | Unmanned aerial vehicle escape route planning | |
EP3260818A1 (en) | System and method for providing aircraft lateral navigation capability feedback to a pilot | |
US11042150B2 (en) | Aircraft fuel efficiency tunnel display for pilots and dispatchers | |
US20190362635A1 (en) | Method and electronic device of management of the display of an aircraft flying profile, associated computer program and electronic system |