Optimal Inverse Simulation of Helicopter Maneuvers
Abstract
An inverse simulation methodology is applied for the optimization of the pirouette and the slalom maneuvers described in the ADS-33 specifications. The optimization process is performed using a genetic algorithm: defined the desired trajectory, the algorithm provides the correct pilot inputs necessary to reproduce the maneuver. The algorithm is based on the maximization of an objective function defined appropriately. A linear model of a BO105 has been used.
[DOI: 10.1685/CSC09261] About DOI
[DOI: 10.1685/CSC09261] About DOI
Keywords
rotorcraft dynamics, ADS-33, maneuvers simulation
Full Text:
PDFDOI: https://doi.org/10.1685/
Except where otherwise noted, content on this site is
licensed under a Creative Commons 2.5 Italy License