Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control
Zhibing Li, Quanlin Dong, Xiaoyue Zhang, Yuanfei Gao
Topics & Concepts
RudderControl theory (sociology)Terminal sliding modeBacksteppingAutopilotSupersonic speedSliding mode controlEngineeringFlight control surfacesAerodynamicsNonlinear systemComputer scienceControl engineeringAdaptive controlControl (management)Aerospace engineeringPhysicsArtificial intelligenceQuantum mechanicsGuidance and Control SystemsAdaptive Control of Nonlinear SystemsMilitary Defense Systems Analysis