The invention provides a UQ-based flight control
servo actuation
system reliability multi-objective optimization method, and relates to the technical field of
aviation system reliability, and the method comprises the following steps: S1, respectively constructing a
system safety optimization objective, a
reliability optimization objective and a
testability optimization objective; s2, constructing a target constraint function based on a security optimization target, a
reliability optimization target and a
testability optimization target, and determining a non-deterministic constraint variable; and S3, solving the target constraint function to obtain an optimized constraint target result. According to the method, uncertainty constraint parameters such as system weight,
material consumption, system redundancy and unit
failure rate are constructed in combination with a
system safety and reliability
testability calculation model for uncertain factors influencing
system safety and reliability testability in a
system design process; and an optimization
algorithm is determined, an optimization solution process is defined, different design schemes and optimization results are obtained through optimization solution, and
collaboration and tradeoff of different
design characteristics of the system are supported.