A formulation of the longitudinal glideslope tracking of a transport-class aircraft in severe wind shear and turbulence for application to robust control system design is presented. Mathematical wind shear models are incorporated into the vehicle mathematical model, and wind turbulence is modeled as an input disturbance signal. For this problem formulation, the horizontal and vertical wind shear gradients are treated as real uncertain parameters that vary over an entire wind shear profile. The primary objective is to examine the formulation of this problem into an appropriate design format for use in m-synthesis control system design
The nonlinear aircraft motion and automatic control model is expanded to incorporate the human pilot...
The definition of a model suitable for certification was the main objective of this report. The mode...
One of the most dangerous parts of the flight is the landing phase, as most accidents occur at this ...
A digital automatic control law to capture a steep glideslope and track the glideslope to a specifie...
One of the most dangerous parts of the flight is the landing phase, as most accidents occur at this ...
Much remains to be learned about the hazards of low altitude wind shear to aviation. New research sh...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
Wind shear is a dangerous condition where there is a sharp change in the direction and magnitude of ...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
Results of studies of wind shear hazard to aircraft operation are summarized. Existing wind shear pr...
A study of intelligent guidance and control concepts for protecting against the adverse effects of w...
Automatic control system design methods for gust and shear alleviation were studied. It is shown tha...
A computational method for modeling severe wind shears of the type that have been documented during ...
The nonlinear aircraft motion and automatic control model is expanded to incorporate the human pilot...
The definition of a model suitable for certification was the main objective of this report. The mode...
One of the most dangerous parts of the flight is the landing phase, as most accidents occur at this ...
A digital automatic control law to capture a steep glideslope and track the glideslope to a specifie...
One of the most dangerous parts of the flight is the landing phase, as most accidents occur at this ...
Much remains to be learned about the hazards of low altitude wind shear to aviation. New research sh...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
Wind shear is a dangerous condition where there is a sharp change in the direction and magnitude of ...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
This paper presents a novel approach to the longitudinal guidance and control issue for an aircraft ...
Results of studies of wind shear hazard to aircraft operation are summarized. Existing wind shear pr...
A study of intelligent guidance and control concepts for protecting against the adverse effects of w...
Automatic control system design methods for gust and shear alleviation were studied. It is shown tha...
A computational method for modeling severe wind shears of the type that have been documented during ...
The nonlinear aircraft motion and automatic control model is expanded to incorporate the human pilot...
The definition of a model suitable for certification was the main objective of this report. The mode...
One of the most dangerous parts of the flight is the landing phase, as most accidents occur at this ...