Aerospace Blockset™Block Reference   1D Controller [A(v),B(v),C(v),D(v)]
  

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1D Controller [A(v),B(v),C(v),D(v)]
1D Controller Blend u=(1-L).K1.y+L.K2.y
1D Observer Form [A(v),B(v),C(v),F(v),H(v)]
1D Self-Conditioned [A(v),B(v),C(v),D(v)]
2D Controller [A(v),B(v),C(v),D(v)]
2D Controller Blend
2D Observer Form [A(v),B(v),C(v),F(v),H(v)]
2D Self-Conditioned [A(v),B(v),C(v),D(v)]
3D Controller [A(v),B(v),C(v),D(v)]
3D Observer Form [A(v),B(v),C(v),F(v),H(v)]
3D Self-Conditioned [A(v),B(v),C(v),D(v)]
3DoF Animation
3DoF (Body Axes)
3DoF (Wind Axes)
3x3 Cross Product
4th Order Point Mass (Longitudinal)
4th Order Point Mass Forces (Longitudinal)
6DoF Animation
6DoF (Euler Angles)
6DoF (Quaternion)
6DoF ECEF (Quaternion)
6DoF Wind (Quaternion)
6DoF Wind (Wind Angles)
6th Order Point Mass (Coordinated Flight)
6th Order Point Mass Forces (Coordinated Flight)
Acceleration Conversion
Adjoint of 3x3 Matrix
Aerodynamic Forces and Moments
Angle Conversion
Angular Acceleration Conversion
Angular Velocity Conversion
Besselian Epoch to Julian Epoch
Calculate Range
CIRA-86 Atmosphere Model
COESA Atmosphere Model
Create 3x3 Matrix
Custom Variable Mass 3DoF (Body Axes)
Custom Variable Mass 3DoF (Wind Axes)
Custom Variable Mass 6DoF (Euler Angles)
Custom Variable Mass 6DoF (Quaternion)
Custom Variable Mass 6DoF ECEF (Quaternion)
Custom Variable Mass 6DoF Wind (Quaternion)
Custom Variable Mass 6DoF Wind (Wind Angles)
Density Conversion
Determinant of 3x3 Matrix
Digital DATCOM Forces and Moments
Direction Cosine Matrix Body to Wind
Direction Cosine Matrix Body to Wind to Alpha and Beta
Direction Cosine Matrix ECEF to NED
Direction Cosine Matrix ECEF to NED to Latitude and Longitude
Direction Cosine Matrix to Quaternions
Direction Cosine Matrix to Rotation Angles
Direction Cosine Matrix to Wind Angles
Discrete Wind Gust Model
Dryden Wind Turbulence Model (Continuous)
Dryden Wind Turbulence Model (Discrete)
Dynamic Pressure
ECEF Position to LLA
EGM96 Geoid
Estimate Center of Gravity
Estimate Inertia Tensor
Flat Earth to LLA
FlightGear Preconfigured 6DoF Animation
Force Conversion
Gain Scheduled Lead-Lag
Generate Run Script
Geocentric to Geodetic Latitude
Geodetic to Geocentric Latitude
Horizontal Wind Model
Ideal Airspeed Correction
Incidence & Airspeed
Incidence, Sideslip & Airspeed
Interpolate Matrix(x)
Interpolate Matrix(x,y)
Interpolate Matrix(x,y,z)
Invert 3x3 Matrix
ISA Atmosphere Model
Julian Epoch to Besselian Epoch
Lapse Rate Model
Length Conversion
LLA to ECEF Position
Mach Number
Mass Conversion
MATLAB Animation
Moments About CG Due to Forces
Non-Standard Day 210C
Non-Standard Day 310
NRLMSISE-00 Atmosphere Model
Pack net_fdm Packet for FlightGear
Pilot Joystick
Pilot Joystick All
Pressure Altitude
Pressure Conversion
Quaternion Conjugate
Quaternion Division
Quaternion Inverse
Quaternion Modulus
Quaternion Multiplication
Quaternion Norm
Quaternion Normalize
Quaternion Rotation
Quaternions to Direction Cosine Matrix
Quaternions to Rotation Angles
Radius at Geocentric Latitude
Relative Ratio
Rotation Angles to Direction Cosine Matrix
Rotation Angles to Quaternions
Second Order Linear Actuator
Second Order Nonlinear Actuator
Self-Conditioned [A,B,C,D]
Send net_fdm Packet to FlightGear
Simple Variable Mass 3DoF (Body Axes)
Simple Variable Mass 3DoF (Wind Axes)
Simple Variable Mass 6DoF (Euler Angles)
Simple Variable Mass 6DoF (Quaternion)
Simple Variable Mass 6DoF ECEF (Quaternion)
Simple Variable Mass 6DoF Wind (Quaternion)
Simple Variable Mass 6DoF Wind (Wind Angles)
Simulation Pace
SinCos
Symmetric Inertia Tensor
Temperature Conversion
Three-Axis Accelerometer
Three-Axis Gyroscope
Three-Axis Inertial Measurement Unit
Turbofan Engine System
Velocity Conversion
Von Karman Wind Turbulence Model (Continuous)
WGS84 Gravity Model
Wind Angles to Direction Cosine Matrix
Wind Angular Rates
Wind Shear Model
World Magnetic Model 2000
World Magnetic Model 2005
  

Block ReferenceBlock Reference 1D Controller [A(v),B(v),C(v),D(v)]1D Controller [A(v),B(v),C(v),D(v)]

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