JSBSim Flight Dynamics Model
1.0 (02 March 2017)
An Open Source Flight Dynamics and Control Software Library in C++
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Runge-Kutta-Fehlberg method. More...
#include <FGRungeKutta.h>
Public Member Functions | |
double | getEpsilon () |
int | getShrinkAvail () |
void | setEpsilon (double e) |
void | setShrinkAvail (int s) |
Public Member Functions inherited from FGRungeKutta | |
void | clearStatus () |
double | evolve (double y_0, FGRungeKuttaProblem *pf) |
double | getError () |
int | getIterations () |
int | getStatus () |
double | getXEnd () |
int | init (double x_start, double x_end, int intervals=4) |
void | setTrace (bool t) |
Additional Inherited Members | |
Public Types inherited from FGRungeKutta | |
enum | eStates { eNoError =0, eMathError =1, eFaultyInit =2, eEvolve =4, eUnknown =8 } |
Protected Attributes inherited from FGRungeKutta | |
double | err |
double | h |
double | h05 |
FGRungeKuttaProblem * | pfo |
Runge-Kutta-Fehlberg method.
This is a semi adaptive implementation of rkf - the interval only shrinks. As a result interval calculations remain trivial, but sometimes too many calculations are performed. Rationale: this code is not meant to be a universal pain-reliever for ode's. Rather it provides some safety if the number of intervals is set too low, or the problem function behaves a bit nasty in rare conditions.
Definition at line 164 of file FGRungeKutta.h.