CN204010285U - A kind of multifunction aircraft telepilot - Google Patents
A kind of multifunction aircraft telepilot Download PDFInfo
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- CN204010285U CN204010285U CN201420355350.5U CN201420355350U CN204010285U CN 204010285 U CN204010285 U CN 204010285U CN 201420355350 U CN201420355350 U CN 201420355350U CN 204010285 U CN204010285 U CN 204010285U
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Abstract
The utility model relates to remote-control aerial field, particularly a kind of multifunction aircraft telepilot.It comprises one-chip computer module, and one-chip computer module is connected with throttle and direction control module, wireless transport module, alarm module, selector switch module, LCD MODULE and gyroscope acceleration module respectively.A kind of multifunction aircraft telepilot of the utility model, has that function is new, cost is low, a feature of simple to operate, low in energy consumption and strong interference immunity, is applicable to the use of operator to various aircraft, also can be applied in remote-control car and remote control ships and light boats field.
Description
Technical field
The utility model relates to remote-control aerial field, particularly a kind of multifunction aircraft telepilot.
Background technology
At present, there is on the market the product of the various telepilots of taking photo by plane, but ubiquity function singleness, feel is bad.The overwhelming majority, is traditional manual operation mode, and along with scientific and technical development, great changes will take place for people life style, this traditional manual operation, can not meet people's needs slowly.People wish a kind of, can be with feeling to control the telepilot of taking photo by plane.
Utility model content
The purpose of this utility model is to provide a kind of multifunction aircraft telepilot.
The purpose of this utility model is achieved through the following channels: a kind of multifunction aircraft telepilot, it comprises one-chip computer module, and one-chip computer module is connected with throttle and direction control module, wireless transport module, alarm module, selector switch module, LCD MODULE and gyroscope acceleration module respectively.
As the further optimization of this programme, the input end ADC0 of described one-chip computer module, ADC1, ADC2, the output terminals A DC0 of ADC3 and throttle and direction control module, ADC1, ADC2, ADC3 is corresponding to be connected, the two-way input/output terminal IRQ of one-chip computer module, MOSI, CSN, MISO, CE, the two-way input/output terminal IRQ of CLK and wireless transport module, MOSI, CSN, MISO, CE, CLK is corresponding to be connected, the output terminal SYSBUZ of one-chip computer module and the corresponding connection of the input end SYSBUZ of alarm module, the input end KEY1 of one-chip computer module and the corresponding connection of the output terminal KEY1 of selector switch module, the two-way input/output terminal OLED_CS of one-chip computer module, OLED_DC, OLED_RW, OLED_RD, OLED_D0, OLED_D1, OLED_D2, OLED_D3, OLED_D4, OLED_D5, OLED_D6, the two-way input/output terminal OLED_CS of OLED_D7 and LCD MODULE, OLED_DC, OLED_RW, OLED_RD, OLED_D0, OLED_D1, OLED_D2, OLED_D3, OLED_D4, OLED_D5, OLED_D6, OLED_D7 is corresponding to be connected, the two-way input/output terminal SCL of one-chip computer module, the two-way input/output terminal SCL of SDA and gyroscope acceleration module, SDA is corresponding to be connected.
As the further optimization of this programme, described one-chip computer module comprises chip U1, the pin 24 of chip U1, pin 36, pin 48 is all connected with stabilized voltage supply end VCC with pin 9, the pin 20 of chip U1 and pin 44 and one end of resistance R 1 and corresponding connection of one end of resistance R 2, the other end of the other end of resistance R 1 and resistance R 2 all with power supply digitally GND_D be connected, chip U1 pin 5 is connected with pin 1 is corresponding with the pin 3 of crystal oscillator Y1 with pin 6, the pin 7 of chip U1 is connected with one end of capacitor C 1 with one end of resistance R 3 respectively, chip U1 pin 8, pin 23, pin 35 and pin 47 all with power supply digitally GND_D be connected, one end of resistance R 3 is connected with one end of K switch 1, the other end of resistance R 3 is connected with stabilized voltage supply end VCC, the other end of the other end of capacitor C 1 and K switch 1 all with power supply digitally GND_D be connected, one end of one end of capacitor C 2 and capacitor C 3 is connected with pin 3 is corresponding with the pin 1 of crystal oscillator Y1, the other end of the other end of capacitor C 2 and capacitor C 3 all with power supply digitally GND_D be connected, capacitor C 4, one end of capacitor C 5 and capacitor C 6 is all connected with stabilized voltage supply end VCC, capacitor C 4, the other end of capacitor C 5 and capacitor C 6 all with power supply digitally GND_D be connected,
The input end ADC0 of chip U1, ADC1, ADC2, the output terminals A DC0 of ADC3 and throttle and direction control module, ADC1, ADC2, ADC3 is corresponding to be connected, the output terminal CSN of chip U1, MOSO, the input end CSN of CE and CLK and wireless transport module, MOSO, CE is connected with CLK is corresponding, the input end IRQ of chip U1 and output terminal IRQ with MOSI corresponding be connected of MOSI with wireless transport module, the output terminal SYSBUZ of chip U1 and the corresponding connection of the input end SYSBUZ of alarm module, the input end KEY1 of chip U1 and the corresponding connection of the output terminal KEY1 of selector switch module, the two-way input/output terminal OLED_CS of chip U1, OLED_DC, OLED_RW, the two-way input/output terminal OLED_CS of OLED_RD and LCD MODULE, OLED_DC, OLED_RW, OLED_RD, output terminal OLED_D0～OLED_D7 of chip U1 and the corresponding connection of the input end OLED_D0～OLED_D7 of LCD MODULE, the output terminal SCL of chip U1 is connected with the input end SCL of gyroscope acceleration module, and the two-way input/output terminal SDA of chip U1 is connected with the two-way input/output terminal SDA of gyroscope acceleration module.
Further optimization as this programme, described throttle and direction control module consist of 2 separate potentiometer P1, P2 of throttle and 2 separate potentiometer P3, P4 of direction, 1 pin of each potentiometer is all connected with GND_M in analog, 3 pin of each potentiometer are connected with stabilized voltage supply end VCC, 2 pin of each potentiometer respectively with C7, C8, the corresponding connection of C9, C10; The corresponding connection of input end ADC0, ADC1, ADC2, ADC3 of output terminals A DC0, the ADC1 of described 1, P2, P3, P4, ADC2, ADC3 and one-chip computer module.
As the further optimization of this programme, described LCD MODULE comprises display screen U4, the pin 1 of display screen U4, pin 8, pin 29, pin 30, one end of resistance R 6, one end of resistance R 10, one end of capacitor C 14, one end of capacitor C 15, one end of capacitor C 16, one end of capacitor C 17 be digitally connected, pin 6, pin 9, one end of resistance R 7, one end of resistance R 8, one end of resistance R 9 is connected with stabilized voltage supply end VCC, pin 2 is connected with capacitor C 12 one end, pin 3 is connected with the other one end of capacitor C 12, pin 4 is connected with capacitor C 13 one end, pin 5 is connected with the other one end of capacitor C 13, pin 10 is connected with other one end of resistance R 6, pin 11 is connected with other one end of resistance R 7, pin 12 is connected with other one end of resistance R 8, other one end of resistance R 9, other one end of capacitor C 17 is connected with pin 14, pin 26 is connected with other one end of resistance R 10, pin 27 is connected with other one end of capacitor C 14, other one end of capacitor C 15, other one end of capacitor C 16 is connected with pin 28, the corresponding connection of two-way input/output terminal OLED_CS, OLED_DC, OLED_RW, OLED_RD of two-way input/output terminal OLED_CS, the OLED_DC of display screen U4, OLED_RW, OLED_RD and one-chip computer module, input end OLED_D0～OLED_D7 of display screen U4 and the corresponding connection of the output terminal OLED_D0～OLED_D7 of one-chip computer module.
As the further optimization of this programme, described gyroscope acceleration module comprises conformability 6 axle motion process assembly U3, the pin 23 of conformability 6 axle motion process assembly U3, pin 24, pin 13, pin 20, one end of pin 10 and pin 8 and resistance R 12, one end of resistance R 11, one end of capacitor C 20, one end of capacitor C 18, the corresponding connection of one end of one end of capacitor C 19 and capacitor C 21, one end of capacitor C 20, one end of capacitor C 21, the other end of the other end of resistance R 11 and resistance R 12 is all connected with stabilized voltage supply end VCC, conformability 6 axle motion process assemblies, the pin 9 of U3, pin 11, pin 18, pin 22, the other end of capacitor C 18, the other end of the other end of capacitor C 19 and capacitor C 20 all with power supply in analog GND_M be connected, the other end of capacitor C 21 and power supply digitally GND_D are connected, the input end SCL of conformability 6 axle motion process assembly U3 is connected with the output terminal SCL of one-chip computer module, and the two-way input/output terminal SDA of conformability 6 axle motion process assembly U3 is connected with the two-way input/output terminal SDA of one-chip computer module.
A kind of multifunction aircraft telepilot of the utility model, has that function is new, cost is low, a feature of simple to operate, low in energy consumption and strong interference immunity, is applicable to the use of operator to various aircraft, also can be applied in remote-control car and remote control ships and light boats field.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is described in further detail:
Fig. 1 is the utility model frame structure schematic diagram;
Fig. 2 is the utility model electrical block diagram;
Fig. 3 is the circuit diagram of one-chip computer module in the utility model;
Fig. 4 is the circuit diagram of throttle and direction control module in the utility model;
Fig. 5 is the circuit diagram of wireless transport module in the utility model;
Fig. 6 is the circuit diagram of alarm module in the utility model;
Fig. 7 is the circuit diagram of selector switch module in the utility model;
Fig. 8 is the circuit diagram of LCD MODULE in the utility model;
Fig. 9 is the circuit diagram of gyroscope acceleration module in the utility model;
In figure, one-chip computer module 1, throttle and direction control module 2, wireless transport module 3, alarm module 4, selector switch module 5, LCD MODULE 6, gyroscope acceleration module 7.
Embodiment
As shown in Figure 1, a kind of multifunction aircraft telepilot of the utility model, it comprises one-chip computer module 1, and one-chip computer module 1 is connected with throttle and direction control module 2, wireless transport module 3, alarm module 4, selector switch module 5, LCD MODULE 6 and gyroscope acceleration module 7 respectively.
As shown in Fig. 2-Fig. 9, the input end ADC0 of described one-chip computer module 1, ADC1, ADC2, the output terminals A DC0 of ADC3 and throttle and direction control module 2, ADC1, ADC2, ADC3 is corresponding to be connected, the two-way input/output terminal IRQ of one-chip computer module 1, MOSI, CSN, MISO, CE, the two-way input/output terminal IRQ of CLK and wireless transport module 3, MOSI, CSN, MISO, CE, CLK is corresponding to be connected, the output terminal SYSBUZ of one-chip computer module 1 and the corresponding connection of the input end SYSBUZ of alarm module 4, the input end KEY1 of one-chip computer module 1 and the corresponding connection of the output terminal KEY1 of selector switch module 5, the two-way input/output terminal OLED_CS of one-chip computer module 1, OLED_DC, OLED_RW, OLED_RD, OLED_D0, OLED_D1, OLED_D2, OLED_D3, OLED_D4, OLED_D5, OLED_D6, the two-way input/output terminal OLED_CS of OLED_D7 and LCD MODULE 6, OLED_DC, OLED_RW, OLED_RD, OLED_D0, OLED_D1, OLED_D2, OLED_D3, OLED_D4, OLED_D5, OLED_D6, OLED_D7 is corresponding to be connected, the two-way input/output terminal SCL of one-chip computer module 1, the two-way input/output terminal SCL of SDA and gyroscope acceleration module 7, SDA is corresponding to be connected.
As shown in Figure 3, described one-chip computer module 1 comprises chip U1, the pin 24 of chip U1, pin 36, pin 48 is all connected with stabilized voltage supply end VCC with pin 9, the pin 20 of chip U1 and pin 44 and one end of resistance R 1 and corresponding connection of one end of resistance R 2, the other end of the other end of resistance R 1 and resistance R 2 all with power supply digitally GND_D be connected, chip U1 pin 5 is connected with pin 1 is corresponding with the pin 3 of crystal oscillator Y1 with pin 6, the pin 7 of chip U1 is connected with one end of capacitor C 1 with one end of resistance R 3 respectively, chip U1 pin 8, pin 23, pin 35 and pin 47 all with power supply digitally GND_D be connected, one end of resistance R 3 is connected with one end of K switch 1, the other end of resistance R 3 is connected with stabilized voltage supply end VCC, the other end of the other end of capacitor C 1 and K switch 1 all with power supply digitally GND_D be connected, one end of one end of capacitor C 2 and capacitor C 3 is connected with pin 3 is corresponding with the pin 1 of crystal oscillator Y1, the other end of the other end of capacitor C 2 and capacitor C 3 all with power supply digitally GND_D be connected, capacitor C 4, one end of capacitor C 5 and capacitor C 6 is all connected with stabilized voltage supply end VCC, capacitor C 4, the other end of capacitor C 5 and capacitor C 6 all with power supply digitally GND_D be connected,
The input end ADC0 of chip U1, ADC1, ADC2, the output terminals A DC0 of ADC3 and throttle and direction control module 2, ADC1, ADC2, ADC3 is corresponding to be connected, the output terminal CSN of chip U1, MOSO, the input end CSN of CE and CLK and wireless transport module 3, MOSO, CE is connected with CLK is corresponding, the input end IRQ of chip U1 and output terminal IRQ with MOSI corresponding be connected of MOSI with wireless transport module 1, the output terminal SYSBUZ of chip U1 and the corresponding connection of the input end SYSBUZ of alarm module 4, the input end KEY1 of chip U1 and the corresponding connection of the output terminal KEY1 of selector switch module 5, the two-way input/output terminal OLED_CS of chip U1, OLED_DC, OLED_RW, the two-way input/output terminal OLED_CS of OLED_RD and LCD MODULE 6, OLED_DC, OLED_RW, OLED_RD, output terminal OLED_D0～OLED_D7 of chip U1 and the corresponding connection of the input end OLED_D0～OLED_D7 of LCD MODULE 6, the output terminal SCL of chip U1 is connected with the input end SCL of gyroscope acceleration module 7, and the two-way input/output terminal SDA of chip U1 is connected with the two-way input/output terminal SDA of gyroscope acceleration module 7.
As shown in Figure 4, described throttle and direction control module 2 consist of 2 separate potentiometer P1, P2 of throttle and 2 separate potentiometer P3, P4 of direction, 1 pin of each potentiometer is all connected with GND_M in analog, 3 pin of each potentiometer are connected with stabilized voltage supply end VCC, 2 pin of each potentiometer respectively with C7, C8, the corresponding connection of C9, C10; The corresponding connection of input end ADC0, ADC1, ADC2, ADC3 of output terminals A DC0, the ADC1 of described 1, P2, P3, P4, ADC2, ADC3 and one-chip computer module 1.
As shown in Figure 8, described LCD MODULE 6 comprises display screen U4, the pin 1 of display screen U4, pin 8, pin 29, pin 30, one end of resistance R 6, one end of resistance R 10, one end of capacitor C 14, one end of capacitor C 15, one end of capacitor C 16, one end of capacitor C 17 be digitally connected, pin 6, pin 9, one end of resistance R 7, one end of resistance R 8, one end of resistance R 9 is connected with stabilized voltage supply end VCC, pin 2 is connected with capacitor C 12 one end, pin 3 is connected with the other one end of capacitor C 12, pin 4 is connected with capacitor C 13 one end, pin 5 is connected with the other one end of capacitor C 13, pin 10 is connected with other one end of resistance R 6, pin 11 is connected with other one end of resistance R 7, pin 12 is connected with other one end of resistance R 8, other one end of resistance R 9, other one end of capacitor C 17 is connected with pin 14, pin 26 is connected with other one end of resistance R 10, pin 27 is connected with other one end of capacitor C 14, other one end of capacitor C 15, other one end of capacitor C 16 is connected with pin 28, the corresponding connection of two-way input/output terminal OLED_CS, OLED_DC, OLED_RW, OLED_RD of two-way input/output terminal OLED_CS, the OLED_DC of display screen U4, OLED_RW, OLED_RD and one-chip computer module 1, input end OLED_D0～OLED_D7 of display screen U4 and the corresponding connection of the output terminal OLED_D0～OLED_D7 of one-chip computer module 1.
As shown in Figure 9, described gyroscope acceleration module 7 comprises conformability 6 axle motion process assembly U3, the pin 23 of conformability 6 axle motion process assembly U3, pin 24, pin 13, pin 20, one end of pin 10 and pin 8 and resistance R 12, one end of resistance R 11, one end of capacitor C 20, one end of capacitor C 18, the corresponding connection of one end of one end of capacitor C 19 and capacitor C 21, one end of capacitor C 20, one end of capacitor C 21, the other end of the other end of resistance R 11 and resistance R 12 is all connected with stabilized voltage supply end VCC, conformability 6 axle motion process assemblies, the pin 9 of U3, pin 11, pin 18, pin 22, the other end of capacitor C 18, the other end of the other end of capacitor C 19 and capacitor C 20 all with power supply in analog GND_M be connected, the other end of capacitor C 21 and power supply digitally GND_D are connected, the input end SCL of conformability 6 axle motion process assembly U3 is connected with the output terminal SCL of one-chip computer module 1, and the two-way input/output terminal SDA of conformability 6 axle motion process assembly U3 is connected with the two-way input/output terminal SDA of one-chip computer module 1.
The above; it is only embodiment of the present utility model; but protection domain of the present utility model is not limited to this; any those of ordinary skill in the art are in the disclosed technical scope of the utility model; the variation that can expect without creative work or replacement, within all should being encompassed in protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with the protection domain that claims were limited.
Claims (6)
1. a multifunction aircraft telepilot, it is characterized in that: it comprises one-chip computer module (1), one-chip computer module (1) is connected with throttle and direction control module (2), wireless transport module (3), alarm module (4), selector switch module (5), LCD MODULE (6) and gyroscope acceleration module (7) respectively.
2. a kind of multifunction aircraft telepilot as claimed in claim 1, is characterized in that: the input end ADC0 of described one-chip computer module (1), ADC1, ADC2, the output terminals A DC0 of ADC3 and throttle and direction control module (2), ADC1, ADC2, ADC3 is corresponding to be connected, the two-way input/output terminal IRQ of one-chip computer module (1), MOSI, CSN, MISO, CE, the two-way input/output terminal IRQ of CLK and wireless transport module (3), MOSI, CSN, MISO, CE, CLK is corresponding to be connected, the corresponding connection of input end SYSBUZ of the output terminal SYSBUZ of one-chip computer module (1) and alarm module (4), the corresponding connection of output terminal KEY1 of the input end KEY1 of one-chip computer module (1) and selector switch module (5), the two-way input/output terminal OLED_CS of one-chip computer module (1), OLED_DC, OLED_RW, OLED_RD, OLED_D0, OLED_D1, OLED_D2, OLED_D3, OLED_D4, OLED_D5, OLED_D6, the two-way input/output terminal OLED_CS of OLED_D7 and LCD MODULE (6), OLED_DC, OLED_RW, OLED_RD, OLED_D0, OLED_D1, OLED_D2, OLED_D3, OLED_D4, OLED_D5, OLED_D6, OLED_D7 is corresponding to be connected, the two-way input/output terminal SCL of one-chip computer module (1), the two-way input/output terminal SCL of SDA and gyroscope acceleration module (7), SDA is corresponding to be connected.
3. a kind of multifunction aircraft telepilot as claimed in claim 1 or 2, is characterized in that: described one-chip computer module (1) comprises chip U1, the pin 24 of chip U1, pin 36, pin 48 is all connected with stabilized voltage supply end VCC with pin 9, the pin 20 of chip U1 and pin 44 and one end of resistance R 1 and corresponding connection of one end of resistance R 2, the other end of the other end of resistance R 1 and resistance R 2 all with power supply digitally GND_D be connected, chip U1 pin 5 is connected with pin 1 is corresponding with the pin 3 of crystal oscillator Y1 with pin 6, the pin 7 of chip U1 is connected with one end of capacitor C 1 with one end of resistance R 3 respectively, chip U1 pin 8, pin 23, pin 35 and pin 47 all with power supply digitally GND_D be connected, one end of resistance R 3 is connected with one end of K switch 1, the other end of resistance R 3 is connected with stabilized voltage supply end VCC, the other end of the other end of capacitor C 1 and K switch 1 all with power supply digitally GND_D be connected, one end of one end of capacitor C 2 and capacitor C 3 is connected with pin 3 is corresponding with the pin 1 of crystal oscillator Y1, the other end of the other end of capacitor C 2 and capacitor C 3 all with power supply digitally GND_D be connected, capacitor C 4, one end of capacitor C 5 and capacitor C 6 is all connected with stabilized voltage supply end VCC, capacitor C 4, the other end of capacitor C 5 and capacitor C 6 all with power supply digitally GND_D be connected,
The input end ADC0 of chip U1, ADC1, ADC2, the output terminals A DC0 of ADC3 and throttle and direction control module (2), ADC1, ADC2, ADC3 is corresponding to be connected, the output terminal CSN of chip U1, MOSO, the input end CSN of CE and CLK and wireless transport module (3), MOSO, CE is connected with CLK is corresponding, the input end IRQ of chip U1 and output terminal IRQ with MOSI corresponding be connected of MOSI with wireless transport module (1), the corresponding connection of input end SYSBUZ of the output terminal SYSBUZ of chip U1 and alarm module (4), the corresponding connection of output terminal KEY1 of the input end KEY1 of chip U1 and selector switch module (5), the two-way input/output terminal OLED_CS of chip U1, OLED_DC, OLED_RW, the two-way input/output terminal OLED_CS of OLED_RD and LCD MODULE (6), OLED_DC, OLED_RW, OLED_RD, the corresponding connection of input end OLED_D0～OLED_D7 of output terminal OLED_D0～OLED_D7 of chip U1 and LCD MODULE (6), the output terminal SCL of chip U1 is connected with the input end SCL of gyroscope acceleration module (7), and the two-way input/output terminal SDA of chip U1 is connected with the two-way input/output terminal SDA of gyroscope acceleration module (7).
4. a kind of multifunction aircraft telepilot as claimed in claim 1 or 2, it is characterized in that: described throttle and direction control module (2) consist of 2 separate potentiometer P1, P2 of throttle and 2 separate potentiometer P3, P4 of direction, 1 pin of each potentiometer is all connected with GND_M in analog, 3 pin of each potentiometer are connected with stabilized voltage supply end VCC, 2 pin of each potentiometer respectively with C7, C8, the corresponding connection of C9, C10; The corresponding connection of input end ADC0, ADC1, ADC2, ADC3 of output terminals A DC0, the ADC1 of described 1, P2, P3, P4, ADC2, ADC3 and one-chip computer module (1).
5. a kind of multifunction aircraft telepilot as claimed in claim 1 or 2, is characterized in that: described LCD MODULE (6) comprises display screen U4, the pin 1 of display screen U4, pin 8, pin 29, pin 30, one end of resistance R 6, one end of resistance R 10, one end of capacitor C 14, one end of capacitor C 15, one end of capacitor C 16, one end of capacitor C 17 be digitally connected, pin 6, pin 9, one end of resistance R 7, one end of resistance R 8, one end of resistance R 9 is connected with stabilized voltage supply end VCC, pin 2 is connected with capacitor C 12 one end, pin 3 is connected with the other one end of capacitor C 12, pin 4 is connected with capacitor C 13 one end, pin 5 is connected with the other one end of capacitor C 13, pin 10 is connected with other one end of resistance R 6, pin 11 is connected with other one end of resistance R 7, pin 12 is connected with other one end of resistance R 8, other one end of resistance R 9, other one end of capacitor C 17 is connected with pin 14, pin 26 is connected with other one end of resistance R 10, pin 27 is connected with other one end of capacitor C 14, other one end of capacitor C 15, other one end of capacitor C 16 is connected with pin 28, the corresponding connection of two-way input/output terminal OLED_CS, OLED_DC, OLED_RW, OLED_RD of two-way input/output terminal OLED_CS, the OLED_DC of display screen U4, OLED_RW, OLED_RD and one-chip computer module (1), the corresponding connection of output terminal OLED_D0～OLED_D7 of input end OLED_D0～OLED_D7 of display screen U4 and one-chip computer module (1).
6. a kind of multifunction aircraft telepilot as claimed in claim 1 or 2, is characterized in that: described gyroscope acceleration module (7) comprises conformability 6 axle motion process assembly U3, the pin 23 of conformability 6 axle motion process assembly U3, pin 24, pin 13, pin 20, one end of pin 10 and pin 8 and resistance R 12, one end of resistance R 11, one end of capacitor C 20, one end of capacitor C 18, the corresponding connection of one end of one end of capacitor C 19 and capacitor C 21, one end of capacitor C 20, one end of capacitor C 21, the other end of the other end of resistance R 11 and resistance R 12 is all connected with stabilized voltage supply end VCC, conformability 6 axle motion process assemblies, the pin 9 of U3, pin 11, pin 18, pin 22, the other end of capacitor C 18, the other end of the other end of capacitor C 19 and capacitor C 20 all with power supply in analog GND_M be connected, the other end of capacitor C 21 and power supply digitally GND_D are connected, the input end SCL of conformability 6 axle motion process assembly U3 is connected with the output terminal SCL of one-chip computer module (1), and the two-way input/output terminal SDA of conformability 6 axle motion process assembly U3 is connected with the two-way input/output terminal SDA of one-chip computer module (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420355350.5U CN204010285U (en) | 2014-06-30 | 2014-06-30 | A kind of multifunction aircraft telepilot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420355350.5U CN204010285U (en) | 2014-06-30 | 2014-06-30 | A kind of multifunction aircraft telepilot |
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| Publication Number | Publication Date |
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| CN204010285U true CN204010285U (en) | 2014-12-10 |
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| CN201420355350.5U Expired - Fee Related CN204010285U (en) | 2014-06-30 | 2014-06-30 | A kind of multifunction aircraft telepilot |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105404188A (en) * | 2015-11-30 | 2016-03-16 | 无锡觅睿恪科技有限公司 | Remote controller for controlling of unmanned plane |
-
2014
- 2014-06-30 CN CN201420355350.5U patent/CN204010285U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105404188A (en) * | 2015-11-30 | 2016-03-16 | 无锡觅睿恪科技有限公司 | Remote controller for controlling of unmanned plane |
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