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With the continuous improvement of the launching frequency of vehicles in China and the increase of various types of pre-research models, higher requirements for the testing efficiency of aircraft have been put forward. Because of the different model requirements, people arrangement problem and various design and implement methods, the traditional testing launching and control software can only used to one model. Since the requirements change, huge human recourse and money need to be cost to develop and maintain the software, and it will also bring the difficulties to the software reliability. In order to overcome existing technical deficiencies, researching the configuration design, using the key techniques of generalized interface design and display terminal loading and data displaying method, proposed a configuration display and monitor system based on complex parameters. It reached the generalized goal of one system applies to multiple models, and decreased the difficulties of the controls flexible extension and integration. The system implemented real-time monitor of the aircraft complex parameters and reuse of the system, increased development efficiency very much.