Package uavsim.flightdynamicsmodel

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Description

Class Summary

A_ControlInput	Defines the shared aspects of a commanded input to the aircraft flight controls.
AircraftModel	Defines a fixed-wing aircraft as a finite-element model consisting of ailerons, flaps, an elevator, a rudder, and a fuselage.
AircraftModelController	Defines the basic inputs to the control surfaces of the aircraft, which in turn modify its state with respect to the flight-dynamics model.
AircraftRigidBody	Defines the rigid-body model of an aircraft.
AircraftRigidBodyElement	Defines a single element of the finite-element model of the rigid-body model of an aircraft.
ControlInputAileron	Defines zzz under construction
ControlInputElevator	Defines zzz under construction
ControlInputFlaps	Defines zzz under construction
ControlInputPower	Defines zzz under construction
ControlInputRudder	Defines zzz under construction
HistoryEntry<_ELEMENT_>	Defines a time-stamped entry for an arbitrary data element.
Matrix	Defines a general-purpose 3x3 mathematical matrix.
Quaternion	Defines a general-purpose mathematical quaternion as an alternative to Euler angles for attitude calculations without singularity limitations at extreme configurations.
Simulation	Defines a simple stub for executing the flight-dynamics model.
Vector	Defines a mathematical vector designed to hold either position (as x, y, and z) or attitude (as roll, pitch, and yaw, respectively).

Package uavsim.flightdynamicsmodel Description

Provides...