Research graph
References from Nonlinear integrated guidance and control based on adaptive backstepping scheme. Local targets link to admitted publications; unresolved targets remain external evidence.
Robust control of linear parametrically varying systems with bounded rates
10.2514/2.4325 · 1998 · External reference
Aeroelastic stability consideration of supersonic flight vehicle using nonlinear aerodynamic response surfaces
10.1016/j.jfluidstructs.2009.04.006 · 2009 · External reference
Aeroelasticity consideration of supersonic vehicle using closed form analytical aerodynamic model
10.1108/00022660910941820 · 2009 · External reference
Integrated design of agile missile guidance and autopilot systems
10.1016/s0967-0661(01)00082-x · 2001 · External reference
Integrated guidance and control of homing missiles against ground fixed targets
10.1016/s1000-9361(08)60021-7 · 2008 · External reference
Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method
1997 · External reference
Gain scheduling for H-infinity controllers: a flight control example
10.1109/87.238400 · 1993 · External reference
Integrated guidance and control for homing missile
2004 · External reference
Dynamic scheduling of modern robust control autopilot designs for missiles
10.1109/37.158896 · 1992 · External reference
A nonlinear stability analysis of elastic flight vehicle
10.1108/00022661211272954 · 2012 · External reference
Integrated guidance and control of elastic flight vehicle based on robust MPC
2014 · External reference
Adaptive integrated guidance and control for missile interceptors
2004 · External reference
Sliding-mode control for integrated missile autopilot guidance
10.2514/1.14951 · 2006 · External reference
Missile longitudinal autopilot design using a new suboptimal nonlinear control method
10.1049/ip-cta:20030966 · 2003 · External reference
Nonlinear H∞ missile longitudinal autopilot design with θ−D method
10.1109/taes.2008.4516988 · 2008 · External reference
Integrated guidance and control of missiles with θ−D method
10.1109/tcst.2006.876903 · 2006 · External reference
Integrated guidance and control for dual-control missiles based on small-gain theorem
10.1016/j.automatica.2012.06.084 · 2012 · External reference
Adaptive integrated guidance and control based on backstepping and input-to-state stability
2013 · External reference
Adaptive multiple sliding surface control for integrated missile guidance and autopilot with terminal angular constraint
2010 · External reference
Effect of estimation on the performance of an integrated missile guidance and control system
10.1109/taes.2011.6034659 · 2011 · External reference
