Integrated guidance and autopilot design for a chasing UAV via high-order sliding modes

DOI10.1016/j.jfranklin.2011.08.004zbMath1254.93059OpenAlexW1985575581MaRDI QIDQ1933447

Takeshi Yamasaki, Hiroyuki Takano, S. N. Balakrishnan

Publication date: 24 January 2013

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2011.08.004

zbMATH Keywords

design synthesishigh-order sliding mode (HOSM) observerintegrated guidance and control (IGC)second-order sliding structureuncertain sliding surfacesUninhabited Aerial Vehicle (UAV)

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Variable structure systems (93B12) Control/observation systems governed by ordinary differential equations (93C15)

Related Items

Research on integrated guidance and control of distributed cooperation of multi-interceptor with state coupling ⋮ Improved off‐policy reinforcement learning algorithm for robust control of unmodeled nonlinear system with asymmetric state constraints ⋮ High-order sliding mode controller design subject to lower-triangular nonlinearity and its application to robotic system ⋮ Projective synchronization of a class of complex network based on high-order sliding mode control ⋮ Design of attitude control system for UAV based on feedback linearization and adaptive control ⋮ Integrated guidance and control with input saturation and impact angle constraint

Cites Work

• Robust exact differentiation via sliding mode technique
• Quasi-continuous high-order sliding-mode controllers