The invention discloses a
radio frequency multi-beam
antenna design method based on multi-objective optimization. The
radio frequency multi-beam
antenna design method comprises the following steps: S1, setting design demand parameters of a spaceborne antenna
system; s2, establishing an antenna structure and electromagnetic performance parameter model, and constructing a corresponding beam forming
network model; s3, an array configuration mode is determined, series feed and parallel feed are combined, and
phase synthesis of the sub-arrays is realized through a
Butler matrix; s4, constructing a multi-objective optimization model, wherein an objective function covers
gain, interval, coverage,
coupling and deployability; s5, sub-array
layout and feed configuration parameters are calculated, and preliminary design is completed; s6, designing an expandable mechanism to ensure folding before launching and on-
orbit unfolding locking; s7,
electromagnetic simulation is carried out, and beam performance is verified; and S8, evaluating a
simulation result, if the
simulation result is not met, returning to optimization, and if the
simulation result is met, outputting a final design scheme. According to the invention, a multi-objective optimization and unfolding structure is integrated, and efficient design and deployment of the
microsatellite multi-beam antenna are realized.