Conference proceeding
Active coning compensation for control of spinning flying vehicles
2010 IEEE International Conference on Control Applications, pp 1832-1837
Sep 2010
Featured in Collection : UN Sustainable Development Goals @ Drexel
Abstract
Many gun launched projectiles spin to maintain in-flight dynamic stability. This spinning often induces the gyroscopic phenomenon known as precession, or coning. Coning poses a problem for actively controlling the projectile. A control scheme is proposed that can compensate for the coning angle of the projectile and allow front-mounted canards to efficiently change the projectile flight path without reaching a stall condition. Closed-loop regulation and H 2 control theories are employed to construct the controller.
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Details
- Title
- Active coning compensation for control of spinning flying vehicles
- Creators
- Mishah Uzziel Salman - Drexel UniversityBorchin Chang - Drexel UniversityIEEE
- Publication Details
- 2010 IEEE International Conference on Control Applications, pp 1832-1837
- Publisher
- IEEE
- Resource Type
- Conference proceeding
- Language
- English
- Academic Unit
- Mechanical Engineering and Mechanics
- Web of Science ID
- WOS:000286943900216
- Scopus ID
- 2-s2.0-78649434891
- Other Identifier
- 991019205314604721
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InCites Highlights
Data related to this publication, from InCites Benchmarking & Analytics tool:
- Web of Science research areas
- Automation & Control Systems
- Engineering, Electrical & Electronic