WO2020136417A2 - Manoeuvring subsystem of unmanned aerial vehicle - Google Patents
Manoeuvring subsystem of unmanned aerial vehicle Download PDFInfo
- Publication number
- WO2020136417A2 WO2020136417A2 PCT/IB2018/060629 IB2018060629W WO2020136417A2 WO 2020136417 A2 WO2020136417 A2 WO 2020136417A2 IB 2018060629 W IB2018060629 W IB 2018060629W WO 2020136417 A2 WO2020136417 A2 WO 2020136417A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aerial vehicle
- unmanned aerial
- manoeuvring
- subsystem
- control unit
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/04—Anti-collision systems
- G08G5/045—Navigation or guidance aids, e.g. determination of anti-collision manoeuvers
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0047—Navigation or guidance aids for a single aircraft
- G08G5/0069—Navigation or guidance aids for a single aircraft specially adapted for an unmanned aircraft
Definitions
- a Manoeuvring Subsystem of an Unmanned Aerial Vehicle which consists of an image sensor to detect obstacles, a control unit which takes input information from the image sensors about one or more obstacles and a system having a gyroscope which takes control signals as input from the above control unit to manoeuvre orientation and angular velocity of the Unmanned Aerial Vehicle to avoid the obstacles.
- Gyroscopic Effect to manoeuvre the Unmanned Aerial Vehicle depending upon the control signal received from the control unit of the Manoeuvring Subsystem.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
Manoeuvring Subsystem Of Unmanned Aerial Vehicle
In this invention we have a Manoeuvring Subsystem of an Unmanned Aerial Vehicle which consists of an image sensor to detect obstacles, a control unit which takes input information from the image sensors about one or more obstacles and a system having a gyroscope which takes control signals as input from the above control unit to manoeuvre orientation and angular velocity of the Unmanned Aerial Vehicle to avoid the obstacles. Here we can use Gyroscopic Effect to manoeuvre the Unmanned Aerial Vehicle depending upon the control signal received from the control unit of the Manoeuvring Subsystem.
Claims
1. In this invention we have a Manoeuvring Subsystem of an Unmanned Aerial Vehicle which consists of an image sensor to detect obstacles, a control unit which takes input information from the image sensors about one or more obstacles and a system having a gyroscope which takes control signals as input from the above control unit to manoeuvre orientation and angular velocity of the Unmanned Aerial Vehicle to avoid the obstacles. Here we can use Gyroscopic Effect to manoeuvre the Unmanned Aerial Vehicle depending upon the control signal received from the control unit of the Manoeuvring Subsystem. The above novel technique by which we built a Manoeuvring Subsystem of an Unmanned Aerial Vehicle is the claim for this invention.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/IB2018/060629 WO2020136417A2 (en) | 2018-12-27 | 2018-12-27 | Manoeuvring subsystem of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/IB2018/060629 WO2020136417A2 (en) | 2018-12-27 | 2018-12-27 | Manoeuvring subsystem of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2020136417A2 true WO2020136417A2 (en) | 2020-07-02 |
Family
ID=71130210
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/IB2018/060629 WO2020136417A2 (en) | 2018-12-27 | 2018-12-27 | Manoeuvring subsystem of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| WO (1) | WO2020136417A2 (en) |
-
2018
- 2018-12-27 WO PCT/IB2018/060629 patent/WO2020136417A2/en active Application Filing
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