Guidance Laws With Input Constraints and Actuator Failures
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Publication:2828570
DOI10.1002/ASJC.1199zbMath1348.93093OpenAlexW1940888989MaRDI QIDQ2828570
Publication date: 26 October 2016
Published in: Asian Journal of Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/asjc.1199
Sensitivity (robustness) (93B35) Input-output approaches in control theory (93D25) Control/observation systems governed by ordinary differential equations (93C15)
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Cites Work
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- Fault-tolerant flight control and guidance systems. Practical methods for small unmanned aerial vehicles
- Fuzzy control for electric power steering system with assist motor current input constraints
- \(\mathcal{H}_-/\mathcal{H}_\infty \) fault detection filter design for discrete-time Takagi-Sugeno fuzzy system
- Three-dimensional nonlinearH? guidance law
- Missile Guidance by Three-Dimensional Proportional Navigation
- Active fault‐tolerant control for near space vehicles based on reference model adaptive sliding mode scheme
- Smooth stabilization implies coprime factorization
- Adaptive Integrated Guidance and Control Based on Backstepping and <scp>I</scp>nput‐to‐<scp>S</scp>tate <scp>S</scp>tability
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