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For a aircraft launched in the field, the requirements of equipment deployment in a short time, long distance of launch control, long standby time and safety control instruction uplink function are proposed for the test and control system, design a wireless test and launch control system apply to field environment, through the integration design of ground front equipment and aircraft equipment in conventional test and launch control system, the electrical interface between aircraft and ground equipment become simpler, the deployment speed and reliability of ground devices become higher; The wireless test and launch control distance of test and launch control system is more than 1 km and the safety control instruction uplink distance is up to 100 km through spread spectrum wireless uplink and FM wireless downlink, the uplink is compatible with conventional safety control uplink; The aircraft can low power hibernation for a long time and launched quickly after wake up in launching site through improvement of aircraft data link and flight control computer; After improvement the ground data link adapt to the field environment when send wireless instruction and receive telemetering data; Design multilevel aircraft initiating explosive circuit and engine ignition circuit control mechanism to ensure the safety of aircraft in storage, transportation and measurement. Through flight test verify that the wireless test and launch control system satisfies the requirements of aircraft launch in field environment.