CONTROL SYSTEM AND STRATEGY FOR TAIL SITTER

摘要

A tail sitter aircraft (10) is capable of forward flight and hover operations. The tail sitter aircraft (10) includes a wing (12, 13) and first (14) and second (15) prop-nacelles supportively disposed on the wing. Each of the first and second prop-nacelles includes an articulable rotor (20), which is rotatable about variable rotational axes and which includes blades (22) that are collectively and cyclically controllable in both forward flight and hover regimes.