Input-output invertibility and sliding mode control for close formation flying of multiple UAVs

DOI<link itemprop=identifier href="https://doi.org/10.1002/1099-1239(200008)10:10<779::AID-RNC513>3.0.CO;2-6" /><779::AID-RNC513>3.0.CO;2-6 10.1002/1099-1239(200008)10:10<779::AID-RNC513>3.0.CO;2-6zbMath0953.93543OpenAlexW2118419116MaRDI QIDQ4508614

Steve Rasmussen, Sahjendra N. Singh, Phil Chandler, Meir Pachter, Corey Schumacher, Siva S. Banda

Publication date: 30 January 2001

Full work available at URL: https://doi.org/10.1002/1099-1239(200008)10:10<779::aid-rnc513>3.0.co;2-6

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable structure systems (93B12)

Related Items (3)

Fault-tolerant formation control of multiple UAVs in the presence of actuator faults ⋮ Retrofit fault‐tolerant tracking control design of an unmanned quadrotor helicopter considering actuator dynamics ⋮ Optimal UAV formation guidance laws with timing constraint

Cites Work

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• Application of nonlinear transformations to automatic flight control
• Flight control design using non-linear inverse dynamics
• Nonlinear flight test trajectory controllers for aircraft
• A calculus for computing Filippov's differential inclusion with application to the variable structure control of robot manipulators
• Invertibility and trajectory control for nonlinear maneuvers of aircraft

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