Testing
Module Product-1
Every little and every little thing
- Function
Executing main control commands: Receives attitude commands from the main control module, precisely drives the corresponding motors, and achieves stable flight.
Independent local control: Closed-loop control of mounted gimbal heads, cameras, spray valves, and other task equipment.
Preprocessing and distribution: Local sensor data (such as ESC temperature, radar obstacle avoidance information) is collected and initially processed before being sent to the main controller, reducing the computational load on the main controller.
- Advantages
Redundancy and fault tolerance: Core components can be designed with "triple redundancy"; if one sub-control module fails, other modules can maintain basic posture and gain emergency return time.
Flexible expansion: Modular design allows easy installation of millimeter-wave radar or multispectral cameras via reserved interfaces.
Reduced latency: Tasks such as motor control are completed locally on the module, without relying on the main controller or communication bus, resulting in faster response.
Easy maintenance: replace any module that malfunctions, without replacing the entire flight control board.
- Technology
Communication protocols: Modules often use CAN bus (high bandwidth, anti-interference) or serial communication.
Clock synchronization: Multiple modules must strictly synchronize the time (usually less than 1 millisecond), otherwise flight control will become chaotic.
Hardware composition: The core is usually an ARM Cortex-M series microcontroller (such as STM32F4/F7), paired with PWM output to drive ESC, and ADC to collect voltage and current.
Module Product-2
Amplify V
- Function
Executing main control commands: Receives attitude commands from the main control module, precisely drives the corresponding motors, and achieves stable flight.
Independent local control: Closed-loop control of mounted gimbal heads, cameras, spray valves, and other task equipment.
Preprocessing and distribution: Local sensor data (such as ESC temperature, radar obstacle avoidance information) is collected and initially processed before being sent to the main controller, reducing the computational load on the main controller.
- Advantages
Redundancy and fault tolerance: Core components can be designed with "triple redundancy"; if one sub-control module fails, other modules can maintain basic posture and gain emergency return time.
Flexible expansion: Modular design allows easy installation of millimeter-wave radar or multispectral cameras via reserved interfaces.
Reduced latency: Tasks such as motor control are completed locally on the module, without relying on the main controller or communication bus, resulting in faster response.
Easy maintenance: replace any module that malfunctions, without replacing the entire flight control board.
- Technology
Communication protocols: Modules often use CAN bus (high bandwidth, anti-interference) or serial communication.
Clock synchronization: Multiple modules must strictly synchronize the time (usually less than 1 millisecond), otherwise flight control will become chaotic.
Hardware composition: The core is usually an ARM Cortex-M series microcontroller (such as STM32F4/F7), paired with PWM output to drive ESC, and ADC to collect voltage and current.
Module Product-3
ddddddd
- Function
Executing main control commands: Receives attitude commands from the main control module, precisely drives the corresponding motors, and achieves stable flight.
Independent local control: Closed-loop control of mounted gimbal heads, cameras, spray valves, and other task equipment.
Preprocessing and distribution: Local sensor data (such as ESC temperature, radar obstacle avoidance information) is collected and initially processed before being sent to the main controller, reducing the computational load on the main controller.
- Advantages
Redundancy and fault tolerance: Core components can be designed with "triple redundancy"; if one sub-control module fails, other modules can maintain basic posture and gain emergency return time.
Flexible expansion: Modular design allows easy installation of millimeter-wave radar or multispectral cameras via reserved interfaces.
Reduced latency: Tasks such as motor control are completed locally on the module, without relying on the main controller or communication bus, resulting in faster response.
Easy maintenance: replace any module that malfunctions, without replacing the entire flight control board.
- Technology
Communication protocols: Modules often use CAN bus (high bandwidth, anti-interference) or serial communication.
Clock synchronization: Multiple modules must strictly synchronize the time (usually less than 1 millisecond), otherwise flight control will become chaotic.
Hardware composition: The core is usually an ARM Cortex-M series microcontroller (such as STM32F4/F7), paired with PWM output to drive ESC, and ADC to collect voltage and current.
Module Product-4
Over and over again
- Function
Executing main control commands: Receives attitude commands from the main control module, precisely drives the corresponding motors, and achieves stable flight.
Independent local control: Closed-loop control of mounted gimbal heads, cameras, spray valves, and other task equipment.
Preprocessing and distribution: Local sensor data (such as ESC temperature, radar obstacle avoidance information) is collected and initially processed before being sent to the main controller, reducing the computational load on the main controller.
- Advantages
Redundancy and fault tolerance: Core components can be designed with "triple redundancy"; if one sub-control module fails, other modules can maintain basic posture and gain emergency return time.
Flexible expansion: Modular design allows easy installation of millimeter-wave radar or multispectral cameras via reserved interfaces.
Reduced latency: Tasks such as motor control are completed locally on the module, without relying on the main controller or communication bus, resulting in faster response.
Easy maintenance: replace any module that malfunctions, without replacing the entire flight control board.
- Technology
Communication protocols: Modules often use CAN bus (high bandwidth, anti-interference) or serial communication.
Clock synchronization: Multiple modules must strictly synchronize the time (usually less than 1 millisecond), otherwise flight control will become chaotic.
Hardware composition: The core is usually an ARM Cortex-M series microcontroller (such as STM32F4/F7), paired with PWM output to drive ESC, and ADC to collect voltage and current.
Module product-5
gfghj
- Function
Executing main control commands: Receives attitude commands from the main control module, precisely drives the corresponding motors, and achieves stable flight.
Independent local control: Closed-loop control of mounted gimbal heads, cameras, spray valves, and other task equipment.
Preprocessing and distribution: Local sensor data (such as ESC temperature, radar obstacle avoidance information) is collected and initially processed before being sent to the main controller, reducing the computational load on the main controller.
- Advantages
Redundancy and fault tolerance: Core components can be designed with "triple redundancy"; if one sub-control module fails, other modules can maintain basic posture and gain emergency return time.
Flexible expansion: Modular design allows easy installation of millimeter-wave radar or multispectral cameras via reserved interfaces.
Reduced latency: Tasks such as motor control are completed locally on the module, without relying on the main controller or communication bus, resulting in faster response.
Easy maintenance: replace any module that malfunctions, without replacing the entire flight control board.
- Technology
Communication protocols: Modules often use CAN bus (high bandwidth, anti-interference) or serial communication.
Clock synchronization: Multiple modules must strictly synchronize the time (usually less than 1 millisecond), otherwise flight control will become chaotic.
Hardware composition: The core is usually an ARM Cortex-M series microcontroller (such as STM32F4/F7), paired with PWM output to drive ESC, and ADC to collect voltage and current.
- 模块产品-6
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- 功能
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执行主控指令：接收主控模块的姿态指令，精确驱动对应的电机，实现稳定飞行。
独立本地控制：对挂载的云台、相机、喷洒阀门等任务设备进行闭环控制。
预处理与分发：采集本地的传感器数据（如电调温度、雷达避障信息），初步处理后发给主控，减轻主控的运算压力。
- 优势
冗余与容错：核心部件可设计为“三余度”，如果一个分控模块失效，其他模块能维持基本姿态，争取紧急返航时间。
灵活扩展：模块化设计，通过预留接口就能轻松加装毫米波雷达或多光谱相机。
降低延迟：电机控制等任务在模块本地完成，不依赖主控和通信总线，响应更快。
便于维护：哪个模块出问题就换哪个，无需更换整块飞控板。
- 技术
通信协议：模块间多采用CAN总线（高带宽、抗干扰）或串口通信。
时钟同步：多模块必须严格同步时间（通常小于1毫秒），否则飞控会紊乱。
硬件构成：核心通常是ARM Cortex-M系列单片机（如STM32F4/F7），搭配PWM输出驱动电调，以及ADC采集电压电流。
