Table 1 The number of vulnerabilities of each subsystem component to EMI in the frequency range of 200 mhz to 5 ghz.
From: Predicting EMI in UAVs using characteristic mode analysis: a case study of the DJI Phantom 4
Antenna | ESC (left, right) | Power interface module | GPS | ESC camera | IMU | Camera | |||||
|---|---|---|---|---|---|---|---|---|---|---|---|
*** | *** | *** | *** | *** | *** | *** | |||||
22 | 12 | 11 | 3 | 4 | 4 | 3 | |||||
*** | ** | ** | ** | *** | *** | *** | |||||
26 | 23 | 8 | 1 | 3 | 2 | 2 | |||||
* | * | * | * | * | * | * | |||||
16 | 16 | 11 | 8 | 4 | 3 | 2 | |||||
Motors | Main board | Camera board | LED sensors | Gimball main board | Ultrasonic | GPS cover | Gimball power board | ||||
*** | *** | *** | *** | *** | *** | *** | *** | ||||
2 | 1 | 1 | 1 | - | - | - | 1 | ||||
*** | ** | *** | *** | ** | ** | ** | ** | ||||
- | 3 | 5 | 6 | 1 | 2 | 1 | 1 | ||||
* | * | * | * | * | * | * | * | ||||
9 | 16 | 2 | - | 3 | 1 | 2 | 1 | ||||
