Add to ORKGAbstract In this paper, a missile longitudinal autopilot is designed using a new nonlinear contro
Discrete-time designs of flight control systems are required for implementation on missile-borne com...
This paper presents a gain-scheduled design for a missile longitudinal autopilot. The gain-scheduled...
This is the author’s copy of the publication as archived with the DLR’s electronic library a
In this paper, a new nonlinear control synthesis technique, the theta- D method, is employed to desi...
In this paper, a new nonlinear H 1 control technique, called μ¡D H 1 method, is employed to design a...
A missile longitudinal autopilot is designed using a new nonlinear control synthesis technique calle...
In this paper, a new nonlinear control method is used to design a full-envelope, hybrid bank-to-turn...
In this paper, a new nonlinear control method is used to design a full-envelope, hybrid bank-to-turn...
In this dissertation, a nonlinear autopilot design for a medium range bank to turn air-to-air missil...
In this dissertation, a nonlinear autopilot design for a medium range bank to turn air-to-air missil...
This paper presents the simulation in ESL of a non-linear 6 degree-of-freedom missile model with an ...
Abstract- The nonlinearity and coupling of the aerospace vehicle dynamics can be linearized and deco...
The application of a new nonlinear robust control strategy to the design of missile autopilots is pr...
n this paper, three-axis autopilot of a tactical flight vehicle has been designed for surface to air...
The paper deals with robust stabilization of lateral and rolling motions of a skid-to- turn missile ...
Discrete-time designs of flight control systems are required for implementation on missile-borne com...
This paper presents a gain-scheduled design for a missile longitudinal autopilot. The gain-scheduled...
This is the author’s copy of the publication as archived with the DLR’s electronic library a
In this paper, a new nonlinear control synthesis technique, the theta- D method, is employed to desi...
In this paper, a new nonlinear H 1 control technique, called μ¡D H 1 method, is employed to design a...
A missile longitudinal autopilot is designed using a new nonlinear control synthesis technique calle...
In this paper, a new nonlinear control method is used to design a full-envelope, hybrid bank-to-turn...
In this paper, a new nonlinear control method is used to design a full-envelope, hybrid bank-to-turn...
In this dissertation, a nonlinear autopilot design for a medium range bank to turn air-to-air missil...
In this dissertation, a nonlinear autopilot design for a medium range bank to turn air-to-air missil...
This paper presents the simulation in ESL of a non-linear 6 degree-of-freedom missile model with an ...
Abstract- The nonlinearity and coupling of the aerospace vehicle dynamics can be linearized and deco...
The application of a new nonlinear robust control strategy to the design of missile autopilots is pr...
n this paper, three-axis autopilot of a tactical flight vehicle has been designed for surface to air...
The paper deals with robust stabilization of lateral and rolling motions of a skid-to- turn missile ...
Discrete-time designs of flight control systems are required for implementation on missile-borne com...
This paper presents a gain-scheduled design for a missile longitudinal autopilot. The gain-scheduled...
This is the author’s copy of the publication as archived with the DLR’s electronic library a