The invention relates to a teaching experiment device for an aircraft navigation, guidance and control technology, comprising a 
missile-borne controller, a real-time 
task management subsystem, a 
missile body structure, an electric rotary table, a 
user interface subsystem and a student experiment PC (
Personal Computer), wherein all the modules are connected and communicated by adopting a 
serial port, a digital I / O (Input / Output), an 
Ethernet or radio, and the like; the 
missile-borne controller can be arranged in the electric rotary table or the missile body structure and is communicated with the real-time 
task management subsystem through the radio or the 
serial port; and the missile-borne controller and the real-time 
task management subsystem realize the configuration of experimental resources, such as an 
inertial measurement unit, a steering engine, the digital I / O, an equivalent device, the 
serial port, a network port, and the like, through the design of 
software and hardware. The teaching experiment device not only has the experimental functions for a module carrying out the principle demonstration of an aircraft, a sensing device module, an actuating mechanism module, a missile-borne controller module, a 
control system synthesis module, and the like, but also can be used as an experimental platform for a user to carry out independent design and research; and in addition, the teaching experiment device has the advantages of simple and compact structure, low cost, complete content, high function integration degree, easiness and convenience for operation, wide applicationscope, and the like.