CN105759828B - Aircraft control device and control method based on control command - Google Patents
Aircraft control device and control method based on control command Download PDFInfo
- Publication number
- CN105759828B CN105759828B CN201610215068.0A CN201610215068A CN105759828B CN 105759828 B CN105759828 B CN 105759828B CN 201610215068 A CN201610215068 A CN 201610215068A CN 105759828 B CN105759828 B CN 105759828B
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- aircraft
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- control terminal
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- 238000000034 method Methods 0.000 title claims abstract description 16
- 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 24
- 230000001133 acceleration Effects 0.000 claims description 11
- 230000005540 biological transmission Effects 0.000 claims description 9
- 230000005484 gravity Effects 0.000 claims description 5
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000001680 brushing effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000009987 spinning Methods 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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Catching Or Destruction (AREA)
- Traffic Control Systems (AREA)
Abstract
The invention discloses an aircraft control device and a control method based on a control command. The invention has the beneficial effects that: the method for updating and sharing the operation of the aircraft in real time is provided, the usability of the aircraft is improved, the use threshold of novice is reduced, and meanwhile, the communication and sharing of aircraft lovers are benefited.
Description
Technical Field
The invention relates to the field of aircrafts, in particular to an aircraft control device and method based on control commands.
Background
In order to solve the problem of difficult operation of the aircraft. The prior art is based on the fact that some pre-stored actions are built in the aircraft system: such as tumbling, spinning, etc., to enhance the playability of the aircraft. However, the operation is single, the new operation can be realized only by brushing the machine, and the operation is complex.
Disclosure of Invention
The invention provides an aircraft control device and a control method based on control commands, aiming at the technical problems in the related art, so as to solve the problems in the prior art.
In order to achieve the technical purpose, the technical scheme of the invention is realized as follows:
the aircraft control device based on the control command comprises an intelligent control terminal, a flight control, a memory and a coprocessor, wherein the intelligent control terminal is connected with the flight control, the flight control is connected with the memory and the coprocessor, and the memory is connected with the coprocessor.
Further, the flight control comprises an acceleration sensor, a gravity sensor and a GPS sensor.
Further, the intelligent control terminal is a mobile phone or a tablet personal computer.
Further, the memory is a nonvolatile memory.
The control method of the aircraft sequentially comprises the steps of controlling the flight action record of the aircraft and controlling the flight action transmission of the aircraft;
wherein: the control of the flight action record of the aircraft comprises the following steps:
1) The intelligent control terminal indicates the aircraft to enter a recording mode, at the moment, the flight control records data sent by the intelligent control terminal, the data comprise PWM values, acceleration sensor states and GPS data in each control period, the serial number of the current period is used as a time stamp, and the coprocessor records control information sent by the intelligent control terminal in real time and records the control information on a nonvolatile memory;
2) After the recording is finished, the intelligent control terminal is required to instruct the aircraft to exit the recording mode, at the moment, the flight control and the coprocessor stop recording, and the recorded data is marked as a complete record;
the control of the flight motion transmission of the aircraft comprises the following steps:
1) When the unmanned plane is in a non-flight state, the coprocessor transmits data recorded during flight action recording of the unmanned plane to the intelligent control terminal;
2) The intelligent control terminal analyzes the data, intercepts data sent by the user controller according to the state of the acceleration sensor, optimizes the data according to the acceleration sensor and the gravity sensor, and simulates and displays the dynamic state of the aircraft on the intelligent control terminal;
3) And uploading the recorded data to a memory after the recorded data are recorded by a user, and sharing the recorded data to a network or storing the recorded data to a local place.
Further, the control method of the aircraft further comprises the step of controlling the replay of the flight actions of the aircraft.
Further, the control of the replay of the flight actions of the aircraft is performed by replaying the flight actions at the intelligent control terminal, and the method comprises the following steps: the intelligent control terminal sequentially transmits the data downloaded or recorded on the internet to the aircraft through the data transmission channel according to the recorded time sequence, and the coprocessor plays back the flight control after receiving the command.
Further, the control of the replay of the flight actions of the aircraft is to replay at the aircraft end, and comprises the following steps: the aircraft pre-stores recorded or downloaded user operations, and the coprocessor informs the flight control of the instruction sequence to re-execute the instruction sequence according to a fixed time sequence according to the instructions of the user.
The invention has the beneficial effects that: the method for updating and sharing the operation of the aircraft in real time is provided, the usability of the aircraft is improved, the use threshold of novice is reduced, and meanwhile, the communication and sharing of aircraft lovers are benefited.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings that are needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic structural view of an aircraft control device based on control commands according to an embodiment of the invention.
In the figure:
1. an intelligent control terminal; 2. flight control; 3. a memory; 4. a coprocessor.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which are derived by a person skilled in the art based on the embodiments of the invention, fall within the scope of protection of the invention.
As shown in fig. 1, an aircraft control device based on a control command according to an embodiment of the present invention includes an intelligent control terminal 1, a flight control 2, a memory 3 and a coprocessor 4, where the intelligent control terminal 1 is connected to the flight control 2, the flight control 2 is connected to the memory 3 and the coprocessor 4, and the memory 3 is connected to the coprocessor 4.
The flight control device comprises a flight control device 2, a storage device 3 and an intelligent control terminal 1, wherein the flight control device 2 comprises an acceleration sensor, a gravity sensor and a GPS sensor, the intelligent control terminal 1 is a mobile phone or a tablet personal computer, and the storage device 3 is a nonvolatile storage device.
The control method of the aircraft sequentially comprises the steps of controlling the flight action record of the aircraft and controlling the flight action transmission of the aircraft;
wherein: the control of the flight action record of the aircraft comprises the following steps:
1) The intelligent control terminal 1 is used for indicating the aircraft to enter a recording mode, at the moment, the flight control 2 of the aircraft records data sent by the intelligent control terminal 1, the data comprise PWM values, acceleration sensor states and GPS data in each control period, the serial number of the current period is used as a time stamp, and meanwhile, the coprocessor 4 records control information sent by the intelligent control terminal 1 in real time and records the control information on a nonvolatile memory;
2) After the recording is finished, the intelligent control terminal 1 is required to instruct the aircraft to exit the recording mode, at the moment, the flight control 2 and the coprocessor 4 of the aircraft stop recording, and the recorded data is marked as a complete record;
the control of the flight motion transmission of the aircraft comprises the following steps:
1) When the unmanned plane is in a non-flight state, the coprocessor 4 transmits data recorded during flight action recording of the unmanned plane to the intelligent control terminal 1;
2) The intelligent control terminal 1 analyzes the data, intercepts the data sent by the user controller according to the state of the acceleration sensor, optimizes the data according to the acceleration sensor and the gravity sensor, and simulates and displays the dynamic state of the aircraft on the intelligent control terminal 1;
3) After being recorded by the user, the data are uploaded to the memory 3 and shared to the network or stored locally.
The control method of the aircraft further comprises the step of controlling the replay of the flight actions of the aircraft;
the control of the replay of the flight actions of the aircraft is performed by the intelligent control terminal 1, and comprises the following steps: the intelligent control terminal 1 sequentially transmits the data downloaded or recorded on the internet to the aircraft through the data transmission channel according to the recorded time sequence, and the coprocessor 4 plays back the flight control 2 of the aircraft after receiving the command.
The control of the replay of the flight actions of the aircraft for the replay at the aircraft end comprises the following steps: the aircraft pre-stores recorded or downloaded user operations, and the coprocessor 4 will inform the flight control 2 of the aircraft that the instruction sequence is re-executed once at a fixed time sequence according to the instructions of the user.
The flight control of the aircraft is a control center of the aircraft and is used for controlling the attitude, the flight state and the like of the aircraft; timestamp: the current time data can be accurately represented; PWM: pulse width modulation is a very effective technique for controlling analog circuits using the digital output of a microprocessor.
The foregoing description of the preferred embodiments of the invention is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the invention.
Claims (1)
1. An aircraft control method based on control commands is characterized in that: the control method of the aircraft sequentially comprises the steps of controlling the flight action record of the aircraft and controlling the flight action transmission of the aircraft; wherein:
the control of the flight action record of the aircraft comprises the following steps:
1) The intelligent control terminal indicates the aircraft to enter a recording mode, at the moment, the flight control records data sent by the intelligent control terminal, the data comprise PWM values, acceleration sensor states and GPS data in each control period, the serial number of the current period is used as a time stamp, and simultaneously, the coprocessor records control information sent by the intelligent control terminal in real time and records the control information on a nonvolatile memory;
2) After the recording is finished, the intelligent control terminal is required to instruct the aircraft to exit the recording mode, at the moment, the flight control and the coprocessor stop recording, and the recorded data is marked as a complete record; the control of the flight motion transmission of the aircraft comprises the following steps:
1) When the unmanned plane is in a non-flight state, the coprocessor transmits data recorded during flight action recording of the unmanned plane to the intelligent control terminal;
2) The intelligent control terminal analyzes the data, intercepts data sent by the user controller according to the state of the acceleration sensor, optimizes the data according to the acceleration sensor and the gravity sensor, and simulates and displays the dynamic state of the aircraft on the intelligent control terminal;
3) After being recorded by a user, the data are uploaded to a memory and shared to a network or stored locally;
the control method of the aircraft further comprises the step of controlling the replay of the flight actions of the aircraft;
the control of the replay of the flight actions of the aircraft is performed by replaying at an intelligent control terminal, and comprises the following steps: the intelligent control terminal sequentially transmits the data downloaded or recorded on the internet to the aircraft through the data transmission channel according to the recorded time sequence, and the coprocessor plays back the flight control after receiving the command;
the control of the replay of the flight actions of the aircraft for the replay at the aircraft end comprises the following steps: the aircraft pre-stores recorded or downloaded user operations, and the coprocessor informs the flight control of the instruction sequence to re-execute the instruction sequence according to a fixed time sequence according to the instructions of the user.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610215068.0A CN105759828B (en) | 2016-04-08 | 2016-04-08 | Aircraft control device and control method based on control command |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610215068.0A CN105759828B (en) | 2016-04-08 | 2016-04-08 | Aircraft control device and control method based on control command |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105759828A CN105759828A (en) | 2016-07-13 |
| CN105759828B true CN105759828B (en) | 2023-10-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610215068.0A Active CN105759828B (en) | 2016-04-08 | 2016-04-08 | Aircraft control device and control method based on control command |
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203773717U (en) * | 2013-11-12 | 2014-08-13 | 武汉大学 | Remote visual touch screen control system for unmanned plane |
| CN104597912A (en) * | 2014-12-12 | 2015-05-06 | 南京航空航天大学 | Tracking flying control system and method of six-rotor unmanned helicopter |
| CN104820428A (en) * | 2015-04-20 | 2015-08-05 | 余江 | Memory type track reproduction method of unmanned aerial vehicle and device |
| CN105070005A (en) * | 2015-07-15 | 2015-11-18 | 合肥佳讯科技有限公司 | Multi-rotor unmanned aerial vehicle and telemetry and telecontrol method |
| CN204871600U (en) * | 2015-05-22 | 2015-12-16 | 刘道满 | Long unmanned aerial vehicle system of time of endurance |
| CN105247593A (en) * | 2014-04-17 | 2016-01-13 | 深圳市大疆创新科技有限公司 | Flight control for flight-restricted regions |
| CN105283816A (en) * | 2013-07-31 | 2016-01-27 | 深圳市大疆创新科技有限公司 | Remote control method and terminal |
| CN205608523U (en) * | 2016-04-08 | 2016-09-28 | 北京米文动力科技有限公司 | Aircraft controlling means based on control command |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016049923A1 (en) * | 2014-09-30 | 2016-04-07 | SZ DJI Technology Co., Ltd. | System and method for data recording and analysis |
-
2016
- 2016-04-08 CN CN201610215068.0A patent/CN105759828B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105283816A (en) * | 2013-07-31 | 2016-01-27 | 深圳市大疆创新科技有限公司 | Remote control method and terminal |
| CN203773717U (en) * | 2013-11-12 | 2014-08-13 | 武汉大学 | Remote visual touch screen control system for unmanned plane |
| CN105247593A (en) * | 2014-04-17 | 2016-01-13 | 深圳市大疆创新科技有限公司 | Flight control for flight-restricted regions |
| CN104597912A (en) * | 2014-12-12 | 2015-05-06 | 南京航空航天大学 | Tracking flying control system and method of six-rotor unmanned helicopter |
| CN104820428A (en) * | 2015-04-20 | 2015-08-05 | 余江 | Memory type track reproduction method of unmanned aerial vehicle and device |
| CN204871600U (en) * | 2015-05-22 | 2015-12-16 | 刘道满 | Long unmanned aerial vehicle system of time of endurance |
| CN105070005A (en) * | 2015-07-15 | 2015-11-18 | 合肥佳讯科技有限公司 | Multi-rotor unmanned aerial vehicle and telemetry and telecontrol method |
| CN205608523U (en) * | 2016-04-08 | 2016-09-28 | 北京米文动力科技有限公司 | Aircraft controlling means based on control command |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105759828A (en) | 2016-07-13 |
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