Self-guiding method for spaceflight test control equipment

The invention discloses a self-guiding method for spaceflight test control equipment. The self-guiding method comprises the following steps of a, starting; b, starting ground spaceflight test controlstation equipment to start to execute a command, initially capturing a target aircraft, and judging whether self-tracking is met or not according to a received state of the target aircraft; c, if a self-tracking condition is satisfied, executing a self-tracking command; d, judging whether the target aircraft is lost or not; e, when the target aircraft is in a lost state, judging whether a trackingmeasurement arc section is ended or not, exiting a task if the arc section is ended, otherwise, entering lost recapture, and judging whether the state of a lost recaptured target aircraft meets self-tracking or not; and f, if the state of the lost recaptured target aircraft meets self-tracking, executing self-tracking, and returning to the step d, otherwise, returning to the step e. According tothe guiding method disclose