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See:
Description
| Class Summary | |
|---|---|
| ADMDynamics | ADMDynamics is an Aircraft which uses a dynamics model to simulate its flight. |
| AircraftDynamics | AircraftDynamics represents the open loop dynamics of the aircraft. |
| AircraftDynamicsResult | This class encapsulates the results that are returned from the AircraftDynamics updateState() method. |
| LateralDerivativeInputs | The following four terms are terms which are supplied as inputs to the LateralDerivatives class. |
| LateralDerivatives | LateralDerivatives is the class that is used to calculate the lateral states of the ADMAircraft. |
| LongitudinalStates | LongitudinalStates is a container that is used to hold the calculated longitudinal state values. |
| Matrix | Matrix is a class that performs common Matrix operations. |
| StateDerivatives | StateDerivatives is the class that is used to calculate the aircraft dynamics states of the aircraft. |
| Exception Summary | |
|---|---|
| MatrixException | MatrixException is thrown when illegal operations are attempted on a Matrix |
This package provides the simulators adm model of the Aircraft's dynamics . It provides a ...
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