The invention discloses a bionic
hummingbird aircraft; a high bionic design is adopted, the unsteady
aerodynamics theory of
hummingbird micro
flapping-wing flight is explored, and a simplified model for realizing the movement law of a vertical take-off and landing and hovering
flapping wing aircraft is established. An ultra-light
flapping-wing
structure based on a five-link
crank rocker and an ultra-light
flapping wing attack angle adjusting structure with a principle similar to a helicopter variable
pitch principle are designed. In accordance with a modular and
integrated design concept, bionic
hummingbird aircraft subsystems such as a
power transmission system and a flight control electronic
system are researched and developed, and a hummingbird
flapping wing prototype vehicle capable ofrealizing switching of vertical
takeoff and landing and hovering flat flight is completed. Based on the design idea of '' flying early and flying more'', an experimental method is used to optimize aniterative principled sample
machine to realize flight maneuvers such as hovering and forward flying of the bionic hummingbird aircraft to achieve the performance requirements of flexible detection. In the future, the bionic hummingbird aircraft can realize multi-bird cluster detection, and complete the low-altitude domain reconnaissance missions in a whole combat area through collaborative control and a bird-
flock-like intelligent
algorithm.