Aircraft correction instruction transmission link design method based on radio frequency integration

The invention discloses an aircraft correction instruction transmission link design method based on radio frequency integration, and the method comprises the steps: (1) carrying out the unified scheduling design of platform radio frequency front-end integration and rear-end integration, the water surface platform L wave band identification function and the aircraft instruction correction function both have the characteristics of instantaneous burst, short duration and low emission duty ratio, and the aircraft instruction correction function and the L wave band identification device antenna are integrated. The L-band identification equipment cabinet receives guidance data and guidance instructions sent by the aircraft instruction correction cabinet through a dual-redundancy broadband Ethernet, and uniformly distributes emission time sequences of instruction correction signals and identification signals according to the principle that aircraft instruction correction is preferential, so that cooperative work of