
基本信息:
- 专利标题: 一种具有姿态调整功能的探空火箭飞控系统
- 专利标题(英):Sounding rocket flight control system with attitude adjustment function
- 申请号:CN201811165986.2 申请日:2018-10-08
- 公开(公告)号:CN109144089A 公开(公告)日:2019-01-04
- 发明人: 李晓明 , 崔敏 , 黄迅 , 林培涵
- 申请人: 五邑大学
- 申请人地址: 广东省江门市蓬江区东成村22号
- 专利权人: 五邑大学
- 当前专利权人: 五邑大学
- 当前专利权人地址: 广东省江门市蓬江区东成村22号
- 代理机构: 广州市红荔专利代理有限公司
- 代理人: 吴伟文
- 主分类号: G05D1/08
- IPC分类号: G05D1/08 ; G05D1/10
The invention relates to a sounding rocket flight control system with an attitude adjustment function, which comprises a main control module, a power supply voltage stabilization module, an ignition module, an attitude adjustment module, a data transmitting and receiving module, an insurance module and a lower computer, wherein the power supply voltage stabilization module, the ignition module, the attitude adjustment module and the data transmitting and receiving module are connected with the main control module, and the lower computer is connected with the data transmitting and receiving module. The sounding rocket flight control system is stable, reliable, low in development cost and high in function expansibility. Compared with the existing small sounding rocket electronic control system, the sounding rocket flight control system adds an attitude adjustment function, can adjust the flight trajectory automatically/manually or compensate disturbance caused by the external environmentthrough the data transmitting and receiving module and the lower computer in the flying process, and is high in adaptability. In addition, 5V voltage is provided for the system through the power supply voltage stabilization module, the safe operation of the system is guaranteed through the insurance module, and the system can carry out response adjustment according to the amplitude of the shakingX and Y axes through two external steering engines.
公开/授权文献:
- CN109144089B 一种具有姿态调整功能的探空火箭飞控系统 公开/授权日:2024-08-13
IPC结构图谱:
G | 物理 |
--G05 | 控制;调节 |
----G05D | 非电变量的控制或调节系统 |
------G05D1/00 | 陆地、水上、空中或太空中的运载工具的位置、航道、高度或姿态的控制,例如自动驾驶仪 |
--------G05D1/08 | .姿态的控制,即摇摆、俯仰角或偏航角的控制 |