A Certain Type Of Rocket Flight Control Software Is Developed

Nowadays under the international situation, a simple control technique make the rocket weapon raise the accuracy of its stroke and effectively cut cost, became the point of rocket weapon in all countries design.This thesis mostly introduce the design and process of fly control software, it is practical problem of project, with difficulty and workload, and some academic investigation. A certain rocket system is weaponry system that lean launch on vehicle lean launch. The objective of investigation is how to design the software of rocket control syetem, that with dependability, security, and precision.This thesis refer to functions realization of of the fly control software.The contents that this thesis mainly studies includes the movement platform, design, test, experiment of software.The main function of software: realtime read data of navigation, make operation of guidance, the attitude control and comprehensive management, and output control signal to rudder machine, and time orders control, fly status search, communication of missile and ground, data of each function module transmission and handle the record instrumen, realization initialization of navigation software before launch, function such as launch and take-off process control...etc.. This requires fully carry out the simulation experiment verify before the design, as possible to consider various possible breakdowns situation, carry on risk analysis, establishment correspond of prepare a case.This thesis refer to tests of the fly control software by developer and third party.This tests find bugs of fly control software,and it advance advice of mend, and make regress test after mend..The result prove that the software is right, and mend is availably.so,it advance validity and dependability of the software.The development of software is according to software engineering austerely.It is make sure that function and capability of the software satisfy requests of software and control system, by various single tests, system tests, assembly tests, confirmation tests. Fly to control developing of software success, provided to guarantee for smoothly developing of a certain rocket aircraft, and make it fly accuracy result to satisfy the demands.