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An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion

  • Published:2013-08 Issue:8 Volume:21 Page:1065-1077
  • ISSN:0967-0661
  • Container-title:Control Engineering Practice
  • language:en
  • Short-container-title:Control Engineering Practice

Author:

Simplício P.,Pavel M.D.,van Kampen E.,Chu Q.P.

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference25 articles.

1. Anonymous (2000). ADS-33E-PRF. United States Army, Aviation and Missile Command.

2. Reconfigurable NDI controller using inertial sensor failure detection & isolation;Bacon;IEEE Transactions on Aerospace and Electronic Systems,2001

3. Bramwell's helicopter dynamics;Bramwell,2001

4. Chen, H. B., & Zhang, S. G. (2008). Robust dynamic inversion flight control law design. In Proceedings of the second international symposium on systems and control in aerospace and astronautics. Shenzhen, China.

5. Dynamic inversion;Enns;International Journal of Control,1994

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