This paper discusses the implementation and simulated performance of the FNPEG (Fully Numerical Predictor-corrector Entry Guidance) algorithm into GNC FSW (Guidance, Navigation, and Control Flight Software) for use in an autonomous re-entry vehicle. A few modifications to FNPEG are discussed that result in computational savings -- a change to the state propagator, and a modification to cross-range lateral logic. Finally, some Monte Carlo results are presented using a representative vehicle in both a high-fidelity 6-DOF (degree-of-freedom) sim as well as in a 3-DOF sim for independent validation.
Automated Re-Entry System using FNPEG
2017
12 pages
Report
Keine Angabe
Englisch
Aircraft , Algorithms , Predictor-corrector methods , Simulation , Automatic landing control , Flight control , Reentry vehicles , Guidance (motion) , Navigation , Autonomy , Measure and integration , Degrees of freedom , Numerical integration , Trajectory planning , Lift drag ratio , Monte carlo method
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