基于STC89C51单片机的气压开伞设计

Design of Model Rocket Automatic Parachute Opener Based on 51 Single Chip Computer

本设计是以模型火箭为设计载体,以STC89C51单片机控制,运用MP085传感芯片、LCD1602显示屏、L298电机的气压开伞设计装置。通过理论分析、模拟仿真,认为该装置下的模型火箭开伞率得以提高。

The design is based on the model rocket as the carrier to STC89C51 single-chip control,the use of MP085 sensor chip,LCD1602 display,L298 motor pressure umbrella as design device.Theoretical analysis and simulation results show that the system has improved the rate of opining parachute.