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An effective flight attitude and trajectory control scheme for sounding rocket
- Source :
- Journal of Physics: Conference Series. 2472:012023
- Publication Year :
- 2023
- Publisher :
- IOP Publishing, 2023.
-
Abstract
- Existing sounding rocket flight is probably disturbed by external factors, of which attitude is lack of automatic control function and flight trajectory is not stable, thus the project designed a canard adjustable posture scheme based on PID control algorithm, which can effectively solve the sounding rocket flight stability and flight path anti-interference problem with high efficiency.
- Subjects :
- History
Computer Science Applications
Education
Subjects
Details
- ISSN :
- 17426596 and 17426588
- Volume :
- 2472
- Database :
- OpenAIRE
- Journal :
- Journal of Physics: Conference Series
- Accession number :
- edsair.doi...........e2d26d3f44df426397dd4b1ac8e1c1e6