A[Aerospace Development & Verification Layer] --> A1[Algorithm modeling, high-altitude scenario calibration, HIL simulation, qualification tests]
B[Powertrain Control Software Layer] --> B1[Motor control, battery management, energy scheduling, thermal management, fault redundancy protection]
C[RapidECU Hardware Control Layer] --> C1[Powertrain control MCU, aviation-grade protected hardware, high-speed bus communication, high-compute main control module]
D[Powertrain Execution & Sensing Layer] --> D1[Traction motors, battery packs, thermal management actuators, voltage/current sensors, speed sensors]
A --> B --> C
C <--> D
C <--> E[Aerospace Command Terminal, Ground Monitoring Platform]
1. Precise motor control: finely regulates motor speed and torque to match different flight conditions and ensure stable power output.
2. Safe battery management: accurately estimates SOC/SOH and performs charging/discharging, balancing and insulation detection to ensure high-altitude battery safety.
3. Intelligent energy scheduling: coordinates energy distribution across components, optimizes utilization efficiency and extends equipment endurance.
4. Integrated thermal management: jointly controls temperatures of the motor, battery and electronic controller to adapt to high/low-temperature cycling.
5. Aerospace-grade protection: complies with aerospace standards; wide-temperature tolerance to cycling, vibration and interference, suited to high-altitude low-pressure conditions.
6. Fault diagnostics and fail-safe protection: monitors component status in real time, handles anomalies by severity, and supports emergency shutdown and alarms.
7. Rapid development and adaptation: based on Simulink graphical modeling with one-click code generation, paired with simulation and calibration tools to shorten tuning cycles.
8. Domestic, classified-data control: fully domestic software and hardware with an encrypted data closed loop, meeting aerospace classified-information requirements.
9. High-altitude condition adaptation: optimizes control strategies for low pressure and high/low-temperature environments to ensure stable operation across all flight altitudes.
1. Integrated hardware/software closed loop: greatly shortens R&D cycles and lowers development cost, enabling rapid conversion from prototype to product.
2. Passes the full set of aerospace environmental tests: reliable across all operating conditions and suited to various flight scenarios.
3. Fully self-controllable hardware and software: core components and algorithms are domestic, meeting domestic-substitution requirements.
4. Modular design: supports interface trimming and function customization for rapid adaptation to various new-energy aerospace equipment.
5. Full-link redundancy: a single-point fault does not affect core functions, improving powertrain safety and reliability.
6. Full-process aerospace engineering services: provides localized technical support and after-sales assurance.
7. High control precision and fast response: precisely meets the refined control needs of new-energy powertrains.