NL2018003B1 - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
- Publication number
- NL2018003B1 NL2018003B1 NL2018003A NL2018003A NL2018003B1 NL 2018003 B1 NL2018003 B1 NL 2018003B1 NL 2018003 A NL2018003 A NL 2018003A NL 2018003 A NL2018003 A NL 2018003A NL 2018003 B1 NL2018003 B1 NL 2018003B1
- Authority
- NL
- Netherlands
- Prior art keywords
- unmanned aerial
- aerial vehicle
- aircraft
- rotor
- main body
- Prior art date
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 50
- 238000000034 method Methods 0.000 description 13
- 230000001133 acceleration Effects 0.000 description 6
- 230000003247 decreasing effect Effects 0.000 description 5
- 238000005096 rolling process Methods 0.000 description 5
- 230000007704 transition Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 238000004891 communication Methods 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 239000000446 fuel Substances 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000009189 diving Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000013178 mathematical model Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 241000282414 Homo sapiens Species 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000011217 control strategy Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 239000002803 fossil fuel Substances 0.000 description 1
- 208000037805 labour Diseases 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012806 monitoring device Methods 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000037221 weight management Effects 0.000 description 1
Classifications
-
- 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
- G05D1/102—Simultaneous control of position or course in three dimensions specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/296—Rotors with variable spatial positions relative to the UAV body
- B64U30/297—Tilting rotors
-
- 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
- G05D1/04—Control of altitude or depth
- G05D1/042—Control of altitude or depth specially adapted for aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
- B64U60/50—Undercarriages with landing legs
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610648326.4A CN106114853B (zh) | 2016-08-09 | 2016-08-09 | 一种无人驾驶航空器 |
Publications (1)
Publication Number | Publication Date |
---|---|
NL2018003B1 true NL2018003B1 (en) | 2017-07-12 |
Family
ID=57258619
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NL2018003A NL2018003B1 (en) | 2016-08-09 | 2016-12-15 | Unmanned aerial vehicle |
Country Status (3)
Country | Link |
---|---|
CN (1) | CN106114853B (de) |
DE (1) | DE202017104421U1 (de) |
NL (1) | NL2018003B1 (de) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109116860A (zh) * | 2018-08-29 | 2019-01-01 | 天津大学 | 三旋翼无人机的非线性鲁棒控制方法 |
CN111522067A (zh) * | 2020-05-25 | 2020-08-11 | 加泰科(深圳)科技有限公司 | 一种基于垂直起降固定翼无人机的海洋航磁探测系统 |
CN113955114A (zh) * | 2021-11-23 | 2022-01-21 | 江苏大学 | 一种基于重心自适应调节装置的直线型无人机结构 |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107315420A (zh) * | 2017-07-01 | 2017-11-03 | 山东翔鸿电子科技有限公司 | 一种无人机转弯方法 |
WO2019056172A1 (zh) * | 2017-09-19 | 2019-03-28 | 深圳市大疆创新科技有限公司 | 无人机的飞行控制方法、无人机及机器可读存储介质 |
EP3587259B1 (de) | 2018-06-28 | 2022-08-10 | Leonardo S.p.A. | Heckstarter und zugehöriges steuerungsverfahren |
CN108873044A (zh) * | 2018-07-05 | 2018-11-23 | 北京航空航天大学 | 一种用gps接收机测直升机螺旋桨相对机身姿态的方法 |
CN109131866A (zh) * | 2018-09-30 | 2019-01-04 | 深圳市旗客智能技术有限公司 | 多轴固定翼复合无人机及其飞行控制方法 |
CN110203387A (zh) * | 2019-05-09 | 2019-09-06 | 深圳市禾启智能科技有限公司 | 垂直起降固定翼飞行器 |
CN110171572B (zh) * | 2019-06-21 | 2024-05-14 | 农业农村部南京农业机械化研究所 | 一种可变形空陆植保无人机 |
CN112166393A (zh) * | 2019-07-30 | 2021-01-01 | 深圳市大疆创新科技有限公司 | 无人飞行器控制方法、控制装置及计算机可读存储介质 |
US20220274701A1 (en) | 2019-08-02 | 2022-09-01 | Aeronext Inc. | Aerial vehicle and flying method of aerial vehicle |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201923320U (zh) * | 2011-01-13 | 2011-08-10 | 杨苡 | 双发动机垂直起降固定翼无人机 |
WO2013012456A2 (en) * | 2011-03-24 | 2013-01-24 | Page Mark Allan | Long endurance vertical takeoff and landing aircraft |
CN103043212B (zh) * | 2011-10-17 | 2016-06-08 | 优利科技有限公司 | 固定翼与电动多旋翼组成的复合飞行器 |
CN202728574U (zh) * | 2011-10-17 | 2013-02-13 | 田瑜 | 固定翼与电动多桨组成的具有直升机功能的复合飞行器 |
US9676488B2 (en) * | 2014-06-10 | 2017-06-13 | Sikorsky Aircraft Corporation | Dual dissimilar engines for an aircraft |
CN204802086U (zh) * | 2015-04-29 | 2015-11-25 | 北京鼎德宝知识产权代理有限公司 | 单人飞行器 |
CN105197237A (zh) * | 2015-09-29 | 2015-12-30 | 上海圣尧智能科技有限公司 | 一种垂直起降无人机 |
-
2016
- 2016-08-09 CN CN201610648326.4A patent/CN106114853B/zh active Active
- 2016-12-15 NL NL2018003A patent/NL2018003B1/en not_active IP Right Cessation
-
2017
- 2017-07-25 DE DE202017104421.1U patent/DE202017104421U1/de not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109116860A (zh) * | 2018-08-29 | 2019-01-01 | 天津大学 | 三旋翼无人机的非线性鲁棒控制方法 |
CN109116860B (zh) * | 2018-08-29 | 2022-05-03 | 天津大学 | 三旋翼无人机的非线性鲁棒控制方法 |
CN111522067A (zh) * | 2020-05-25 | 2020-08-11 | 加泰科(深圳)科技有限公司 | 一种基于垂直起降固定翼无人机的海洋航磁探测系统 |
CN113955114A (zh) * | 2021-11-23 | 2022-01-21 | 江苏大学 | 一种基于重心自适应调节装置的直线型无人机结构 |
Also Published As
Publication number | Publication date |
---|---|
DE202017104421U1 (de) | 2017-09-26 |
CN106114853A (zh) | 2016-11-16 |
CN106114853B (zh) | 2019-05-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PD | Change of ownership |
Owner name: SHANDONG JIANYING INTELLIGENT CONTROL CO. LTD; CN Free format text: DETAILS ASSIGNMENT: CHANGE OF OWNER(S), ASSIGNMENT; FORMER OWNER NAME: CHINA AVIATION MARINE EQUIPMENT (YANTAI) TECHNOLOGY CO. LTD. Effective date: 20191213 |
|
MM | Lapsed because of non-payment of the annual fee |
Effective date: 20210101 |