CN103412568B - Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie - Google Patents

Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie Download PDF

Info

Publication number
CN103412568B
CN103412568B CN201310378368.7A CN201310378368A CN103412568B CN 103412568 B CN103412568 B CN 103412568B CN 201310378368 A CN201310378368 A CN 201310378368A CN 103412568 B CN103412568 B CN 103412568B
Authority
CN
China
Prior art keywords
unmanned plane
flying height
control module
ground
boat
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.)
Active
Application number
CN201310378368.7A
Other languages
Chinese (zh)
Other versions
CN103412568A (en
Inventor
向泽君
梁建国
胡开全
张俊前
周智勇
王快
马红
严以成
骆亮
陈银福
刘超祥
王昌翰
王莉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chongqing Institute Of Surveying And Mapping Science And Technology Chongqing Map Compilation Center
Original Assignee
Chongqing Survey Institute
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Chongqing Survey Institute filed Critical Chongqing Survey Institute
Priority to CN201310378368.7A priority Critical patent/CN103412568B/en
Publication of CN103412568A publication Critical patent/CN103412568A/en
Application granted granted Critical
Publication of CN103412568B publication Critical patent/CN103412568B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

A kind of boat is taken the photograph in unmanned plane aeroplane photography and is become flying height control method with sortie, comprise unmanned plane, unmanned plane during flying height control module, the boat be mounted on unmanned plane take the photograph equipment, its innovation is: in unmanned plane during flying process, carry out dynamic adjustments according to landform height change to the flying height of unmanned plane; Advantageous Effects of the present invention is: under the condition reducing landing number of times, effectively ensures that the ground resolution of image is in better state, meanwhile, also makes the consistance of the ground resolution of the different image in ground better, reduces the difficulty of later stage image processing.

Description

Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie
Technical field
The present invention relates to a kind of unmanned plane that adopts and carry out aerophotographic technology, particularly relate to a kind of with sortie change flying height unmanned aerial vehicle remote sensing images acquisition methods.
Background technology
Undertaking of surveying and mapping, as in social development and economic construction a property in early stage, basic work, is all of great practical significance to the rural-urban integrated planning in area, mountain region and new countryside construction etc.; Unmanned air vehicle technique is the emerging technology of rising in recent years, takes the photograph operation means compared to former boat, and employing unmanned plane carries out navigating taking the photograph and has low cost, easy to operate advantage;
In prior art, unmanned air vehicle technique has been used in mapping operation, but current applied environment is also only limitted to obtain the remote sensing image of plains region, this is mainly because plains region landform is comparatively mild, under the condition not considering weather effect, unmanned plane is when carrying out boat and taking the photograph to plains region, the relative height on unmanned plane and ground can maintain metastable height, the ground resolution obtaining image can be controlled preferably, and interior industry process is relatively easy;
For Mountainous Regions, because topographic relief is larger, the relative height on unmanned plane and ground is dynamic change state, and relative height is the key factor affecting image resolution, therefore, in prior art, when unmanned plane being used for mountain area boat and taking the photograph, the ground resolution ginseng that there is aerial stereo images is secondary uneven, in-and-out situation, this increases not only the difficulty of interior industry Image Matching, and in order to ensure the consistance of ground resolution, need to drive time that the frequent landing unmanned plane in ground carries out differing heights to the same area repeats shooting operation more, troublesome poeration, equipment loss is serious, and drive secondary increase along with taking off, the probability of appearance accident also increases relatively.
Summary of the invention
For the problem in background technology, the present invention proposes a kind of boat to take the photograph in unmanned plane aeroplane photography with sortie change flying height control method, comprise unmanned plane, unmanned plane during flying height control module, the boat be mounted on unmanned plane take the photograph equipment, its innovation is: the lens focus setting described boat to take the photograph equipment as f, pixel dimension be a, and f and a is known quantity; Fly in journey in the single rack time boat of a certain unmanned plane, regulate the flying height of unmanned plane as follows:
1) be preset with theoretical ground resolution GSD in unmanned plane during flying height control module, when just taking off, unmanned plane during flying height control module solves the theoretical relative height H on unmanned plane and ground by following formula, and presses the Initial Flight Level that H regulates unmanned plane:
H = f × GSD a ;
Reach Initial Flight Level and after arriving territory, predetermined air cover, boat is taken the photograph equipment and started working;
2), in unmanned plane during flying process, the flying height of unmanned plane is regulated according to the fluctuating quantity on ground; If before uprising, the flying height of unmanned plane is H0, and the high variable quantity of current landform is h;
3) unmanned plane during flying height control module reads high variable quantity h in real time, if h>0, namely ground elevation increases, then unmanned plane during flying height control module controls unmanned plane increases flying height, if h<0, namely ground elevation reduces, then unmanned plane during flying height control module controls unmanned plane reduction flying height, thus the actual relative height on unmanned plane and ground is maintained near theoretical relative height H all the time, and then ensure that the image resolution obtained is consistent.
After adopting aforementioned schemes, can in unmanned plane during flying process, according to theoretical ground resolution, dynamically regulate the flying height of unmanned plane, make the relative height on unmanned plane and ground maintain metastable state, ensure that ground resolution meets the demands, avoid repeatedly repeating shooting to the same area, also assures that the ground resolution of different image is relatively consistent, the difficulty of industry image processing in reducing simultaneously.For the concrete regulating measure of unmanned plane during flying height, adopt existing unmanned plane during flying attitude control technology to realize, do not repeat them here.
In order to improve the relative stability of the relative height of unmanned plane and ground further, the present invention has also done following improvement: in step 3) when regulating the flying height of unmanned plane, regulates unmanned plane during flying height Δ H as follows:
ΔH=h
If Δ H is negative value, namely ground elevation value reduce, then unmanned plane during flying height control module control unmanned plane flying height reduce | Δ H|, if Δ H be on the occasion of, namely ground elevation value increases, then unmanned plane during flying height control module controls the flying height raising of unmanned plane | Δ H|; In flight course, the practical flight height H 1 of unmanned plane is as follows:
H1=H0+ΔH。
After adopting this to improve, unmanned plane during flying height control module can regulate the flying height of unmanned plane quantitatively according to Δ H, to ensure the flying height controllable precise of unmanned plane.
Cause controlling difficulty to increase in order to avoid frequently regulating flying height, the present invention has also done following improvement: be also preset with ground change altitude datum h in described unmanned plane during flying height control module 0if, h≤h 0, then the flying height of unmanned plane is not regulated, if h > is h 0, then regulate by the flying height of mode in step 3) to unmanned plane.
Based on aforementioned schemes, the invention allows for a kind of with sortie change flying height unmanned aerial vehicle remote sensing images acquisition methods, the steps include:
A, take the photograph project demands according to boat and set theoretical ground resolution;
B, the preliminary survey of basis to actual landform, cook up unmanned plane during flying circuit;
C, when just taking off, solve the theoretical relative height H on unmanned plane and ground by following formula, and press the Initial Flight Level that H regulates unmanned plane:
H = f &times; GSD a ;
Wherein, f is the lens focus that the boat be mounted on unmanned plane takes the photograph equipment, and a is the pixel dimension that the boat be mounted on unmanned plane takes the photograph equipment, and GSD is theoretical ground resolution;
Reach Initial Flight Level and after arriving territory, predetermined air cover, start boat and take the photograph operation;
D, in unmanned plane during flying process, regulate the flying height of unmanned plane according to the fluctuating quantity on ground; If before unmanned plane uprises, the flying height of unmanned plane is H0, and the high variable quantity of current landform is h, and so the regulated value Δ H of unmanned plane during flying height control module to its flying height is as follows:
ΔH=h
If floor level reduce, then h is negative value, if floor level increase, then h be on the occasion of, now can obtain unmanned plane during flying height regulated value Δ H;
When Δ H is negative value, then unmanned plane during flying height control module control unmanned plane flying height reduce | Δ H|, when Δ H be on the occasion of time, then unmanned plane during flying height control module control unmanned plane flying height raising | Δ H|.
Preferably, ground change altitude datum h is preset with in described unmanned plane during flying height control module 0if, h≤h 0, then the flying height of unmanned plane is not regulated, if h > is h 0, then regulate by the flying height of mode in step D to unmanned plane.
Advantageous Effects of the present invention is: under the condition reducing landing number of times, effectively ensures that the ground resolution of image is in better state, meanwhile, also makes the consistance of the ground resolution of the different image in ground better, reduces the difficulty of later stage image processing.
Embodiment
A kind of boat is taken the photograph in unmanned plane aeroplane photography and is become flying height control method with sortie, comprise unmanned plane, unmanned plane during flying height control module, the boat be mounted on unmanned plane take the photograph equipment, its innovation is: the lens focus setting described boat to take the photograph equipment as f, pixel dimension be a, and f and a is known quantity; Fly in journey in the single rack time boat of a certain unmanned plane, regulate the flying height of unmanned plane as follows:
1) be preset with theoretical ground resolution GSD in unmanned plane during flying height control module, when just taking off, unmanned plane during flying height control module solves the theoretical relative height H on unmanned plane and ground by following formula, and presses the Initial Flight Level that H regulates unmanned plane:
H = f &times; GSD a ;
Reach Initial Flight Level and after arriving territory, predetermined air cover, boat is taken the photograph equipment and started working;
2), in unmanned plane during flying process, the flying height of unmanned plane is regulated according to the fluctuating quantity on ground; If before uprising, the flying height of unmanned plane is H0, and the high variable quantity of current landform is h;
3) unmanned plane during flying height control module reads high variable quantity h in real time, if h>0, namely ground elevation increases, then unmanned plane during flying height control module controls unmanned plane increases flying height, if h<0, namely ground elevation reduces, then unmanned plane during flying height control module controls unmanned plane reduction flying height, thus the actual relative height on unmanned plane and ground is maintained near theoretical relative height H all the time, and then ensure that the image resolution obtained is consistent.
Further, in step 3) when regulating the flying height of unmanned plane, regulate unmanned plane during flying height Δ H as follows:
ΔH=h
If Δ H is negative value, namely ground elevation value reduce, then unmanned plane during flying height control module control unmanned plane flying height reduce | Δ H|, if Δ H be on the occasion of, namely ground elevation value increases, then unmanned plane during flying height control module controls the flying height raising of unmanned plane | Δ H|; In flight course, the practical flight height H 1 of unmanned plane is as follows:
H1=H0+ΔH。
Further, ground change altitude datum h is also preset with in described unmanned plane during flying height control module 0if, h≤h 0, then the flying height of unmanned plane is not regulated, if h > is h 0, then regulate by the flying height of mode in step 3) to unmanned plane.
A kind of with sortie change flying height unmanned aerial vehicle remote sensing images acquisition methods, the steps include:
A, take the photograph project demands according to boat and set theoretical ground resolution;
B, the preliminary survey of basis to actual landform, cook up unmanned plane during flying circuit;
C, when just taking off, solve the theoretical relative height H on unmanned plane and ground by following formula, and press the Initial Flight Level that H regulates unmanned plane:
H = f &times; GSD a ;
Wherein, f is the lens focus that the boat be mounted on unmanned plane takes the photograph equipment, and a is the pixel dimension that the boat be mounted on unmanned plane takes the photograph equipment, and GSD is theoretical ground resolution;
Reach Initial Flight Level and after arriving territory, predetermined air cover, start boat and take the photograph operation;
D, in unmanned plane during flying process, regulate the flying height of unmanned plane according to the fluctuating quantity on ground; If before unmanned plane uprises, the flying height of unmanned plane is H0, and the high variable quantity of current landform is h, and so the regulated value Δ H of unmanned plane during flying height control module to its flying height is as follows:
ΔH=h
If floor level reduce, then h is negative value, if floor level increase, then h be on the occasion of, now can obtain unmanned plane during flying height regulated value Δ H;
When Δ H is negative value, then unmanned plane during flying height control module control unmanned plane flying height reduce | Δ H|, when Δ H be on the occasion of time, then unmanned plane during flying height control module control unmanned plane flying height raising | Δ H|.
Further, ground change altitude datum h is preset with in described unmanned plane during flying height control module 0if, h≤h 0, then the flying height of unmanned plane is not regulated, if h > is h 0, then regulate by the flying height of mode in step D to unmanned plane.

Claims (4)

1. a boat is taken the photograph in unmanned plane aeroplane photography and is become flying height control method with sortie, comprise unmanned plane, unmanned plane during flying height control module, the boat be mounted on unmanned plane take the photograph equipment, it is characterized in that: the lens focus setting described boat to take the photograph equipment as f, pixel dimension be a, and f and a is known quantity; Fly in journey in the single rack time boat of a certain unmanned plane, regulate the flying height of unmanned plane as follows:
1) be preset with theoretical ground resolution GSD in unmanned plane during flying height control module, when just taking off, unmanned plane during flying height control module solves the theoretical relative height H on unmanned plane and ground by following formula, and presses the Initial Flight Level that H regulates unmanned plane:
H = f &times; G S D a ;
Reach Initial Flight Level and after arriving territory, predetermined air cover, boat is taken the photograph equipment and started working;
2), in unmanned plane during flying process, the flying height of unmanned plane is regulated according to the fluctuating quantity on ground; If before uprising, the flying height of unmanned plane is H0, and the high variable quantity of current landform is h;
3) unmanned plane during flying height control module reads high variable quantity h in real time, if h>0, namely ground elevation increases, then unmanned plane during flying height control module controls unmanned plane increases flying height, if h<0, namely ground elevation reduces, then unmanned plane during flying height control module controls unmanned plane reduction flying height, thus the actual relative height on unmanned plane and ground is maintained near theoretical relative height H all the time, and then ensure that the image resolution obtained is consistent;
In step 3) when regulating the flying height of unmanned plane, regulate unmanned plane during flying height Δ H as follows:
ΔH=h
If Δ H is negative value, namely ground elevation value reduce, then unmanned plane during flying height control module control unmanned plane flying height reduce | Δ H|, if Δ H be on the occasion of, namely ground elevation value increases, then unmanned plane during flying height control module controls the flying height raising of unmanned plane | Δ H|; In flight course, the practical flight height H 1 of unmanned plane is as follows:
H1=H0+ΔH。
2. boat according to claim 1 is taken the photograph in unmanned plane aeroplane photography and is become flying height control method with sortie, it is characterized in that: be also preset with ground change altitude datum h in described unmanned plane during flying height control module 0if, h≤h 0, then the flying height of unmanned plane is not regulated, if h>h 0, then regulate by the flying height of mode in step 3) to unmanned plane.
3. become a flying height unmanned aerial vehicle remote sensing images acquisition methods with sortie, it is characterized in that:
A, take the photograph project demands according to boat and set theoretical ground resolution;
B, the preliminary survey of basis to actual landform, cook up unmanned plane during flying circuit;
C, when just taking off, solve the theoretical relative height H on unmanned plane and ground by following formula, and press the Initial Flight Level that H regulates unmanned plane:
H = f &times; G S D a ;
Wherein, f is the lens focus that the boat be mounted on unmanned plane takes the photograph equipment, and a is the pixel dimension that the boat be mounted on unmanned plane takes the photograph equipment, and GSD is theoretical ground resolution;
Reach Initial Flight Level and after arriving territory, predetermined air cover, start boat and take the photograph operation;
D, in unmanned plane during flying process, regulate the flying height of unmanned plane according to the fluctuating quantity on ground; If before unmanned plane uprises, the flying height of unmanned plane is H0, and the high variable quantity of current landform is h, and so the regulated value Δ H of unmanned plane during flying height control module to flying height is as follows:
ΔH=h
If floor level reduce, then h is negative value, if floor level increase, then h be on the occasion of, now can obtain unmanned plane during flying height regulated value Δ H;
When Δ H is negative value, then unmanned plane during flying height control module control unmanned plane flying height reduce | Δ H|, when Δ H be on the occasion of time, then unmanned plane during flying height control module control unmanned plane flying height raising | Δ H|.
4. same sortie according to claim 3 becomes flying height unmanned aerial vehicle remote sensing images acquisition methods, it is characterized in that: be preset with ground change altitude datum h in described unmanned plane during flying height control module 0if, h≤h 0, then the flying height of unmanned plane is not regulated, if h>h 0, then regulate by the flying height of mode in step D to unmanned plane.
CN201310378368.7A 2013-08-27 2013-08-27 Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie Active CN103412568B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310378368.7A CN103412568B (en) 2013-08-27 2013-08-27 Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310378368.7A CN103412568B (en) 2013-08-27 2013-08-27 Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie

Publications (2)

Publication Number Publication Date
CN103412568A CN103412568A (en) 2013-11-27
CN103412568B true CN103412568B (en) 2016-01-20

Family

ID=49605593

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310378368.7A Active CN103412568B (en) 2013-08-27 2013-08-27 Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie

Country Status (1)

Country Link
CN (1) CN103412568B (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113238581A (en) * 2016-02-29 2021-08-10 星克跃尔株式会社 Method and system for flight control of unmanned aerial vehicle
CN107108023B (en) * 2016-12-22 2019-09-27 深圳市大疆创新科技有限公司 Unmanned plane and its control method
CN106774406B (en) * 2016-12-30 2023-06-23 武汉大势智慧科技有限公司 Unmanned aerial vehicle image automatic acquisition system and method
CN107065932B (en) * 2017-06-15 2020-04-07 西安电子科技大学 Control method of disaster detection quad-rotor unmanned aerial vehicle
WO2019000323A1 (en) * 2017-06-29 2019-01-03 深圳市大疆创新科技有限公司 Unmanned aerial vehicle and control method therefor, and control terminal and control method therefor
CN108562279B (en) * 2018-03-06 2021-06-22 平湖市城工建设测绘设计有限责任公司 Unmanned aerial vehicle surveying and mapping method
CN109000524B (en) * 2018-08-09 2021-11-05 长安大学 Boundary control blasting method for reducing over-excavation and under-excavation
CN111367302B (en) * 2020-03-03 2023-03-21 大连海洋大学 Unmanned aerial vehicle self-adaptive height-fixing method for offshore cage culture inspection

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19709097A1 (en) * 1997-03-06 1998-10-01 Dornier Gmbh Flight guidance system for low-flying aircraft
CN101067552A (en) * 2007-02-02 2007-11-07 北京航空航天大学 RVSM airspace aeronautical device height holding performance monitoring system and method
CN101270994A (en) * 2008-03-27 2008-09-24 北京航空航天大学 Unmanned aerial vehicle radio-altimeter height and lifting speed self-correcting method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101200913B1 (en) * 2010-05-18 2012-11-13 한국항공우주산업 주식회사 Portable land control apparatus

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19709097A1 (en) * 1997-03-06 1998-10-01 Dornier Gmbh Flight guidance system for low-flying aircraft
CN101067552A (en) * 2007-02-02 2007-11-07 北京航空航天大学 RVSM airspace aeronautical device height holding performance monitoring system and method
CN101270994A (en) * 2008-03-27 2008-09-24 北京航空航天大学 Unmanned aerial vehicle radio-altimeter height and lifting speed self-correcting method

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
固定翼无人机低空遥感系统在山地区域影像获取研究;胡开全等;《北京测绘》;20111231(第3期);全文 *
地形起伏对无人机低空航测影响分析-以东桥镇、龙海市为例;张永年等;《测绘与空间地理信息》;20130331;第36卷(第3期);期刊第176-177页 *
直升机大比例尺航空物探在深部找矿中的应用前景;熊盛青等;《地球科学进展》;20080330;第23卷(第3期);期刊第271页 *

Also Published As

Publication number Publication date
CN103412568A (en) 2013-11-27

Similar Documents

Publication Publication Date Title
CN103412568B (en) Flying height unmanned aerial vehicle remote sensing images acquisition methods is become with sortie
CN107672817A (en) A kind of intelligent landing system of mobile vehicle-mounted unmanned plane
CN106774431B (en) Method and device for planning air route of surveying and mapping unmanned aerial vehicle
CN105549603B (en) A kind of Intelligent road inspection control method of multi-rotor unmanned aerial vehicle
CN104898690A (en) Rotor unmanned aerial vehicle self journey-continuing realization method based on APM platform
CN105468014B (en) A kind of integrated aerocraft system of list autopilot and its two-dimensional pan-tilt control method
CN102806990B (en) Portable type mapping unmanned plane
CN103176475A (en) Ground station for unmanned aerial vehicles
CN105045281A (en) Unmanned aerial vehicle flight control method and device
US20170357255A1 (en) Method for controlling unmanned aerial vehicle using smart device
CN104808666B (en) The method that automatic mobile device extends displacement
CN106155086A (en) A kind of Road Detection unmanned plane and automatic cruising method thereof
CN104590576A (en) Flight control system and method for ship-borne unmanned aerial vehicle autonomous landing
CN107438751B (en) Method and device for detecting flying height and unmanned aerial vehicle
CN109677627B (en) System and method for controlling accurate landing of tethered unmanned aerial vehicle
DE102011086336A1 (en) DEVICE AND METHOD FOR OPERATING A VEHICLE
CN110155350B (en) Control method of unmanned aerial vehicle landing device
CN106292126A (en) A kind of intelligence aerial survey flight exposal control method, unmanned aerial vehicle (UAV) control method and terminal
CN107305395A (en) Unmanned plane method and system
CN109634297A (en) A kind of multi-rotor unmanned aerial vehicle and control method based on light stream sensor location navigation
CN104865969A (en) Control system designing and flight testing method based on unmanned aerial vehicle flight mode
CN104897159A (en) Aircraft full-course navigation method based on sequence image matching
CN112000129A (en) Improved ground-imitating flight control method for unmanned aerial vehicle
WO2015101102A1 (en) Vehicle speed control method and device
CN208715485U (en) A kind of agricultural remote sensing data acquisition equipment equipped with three smooth cameras

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20240320

Address after: No. 6 Qingzhu East Road, Dazhulin Street, Yubei District, Chongqing, 400000

Patentee after: Chongqing Institute of Surveying and Mapping Science and Technology (Chongqing Map Compilation Center)

Country or region after: China

Address before: 400020 Jiangbei District, Chongqing electric measuring Village No. 231

Patentee before: CHONGQING SURVEY INSTITUTE

Country or region before: China

TR01 Transfer of patent right