The invention relates to virtual prototype disassembly
sequence planning technology and provides a virtual prototype disassembly
sequence planning method which mainly aims at solving the problem that high arbitrariness exists in a starting point and a stopping point of disassembly and removal of disassembly restriction in the process of practical maintenance disassembly of a guided
missile device due to different disassembly missions. Due to lack of scientific judgment on a feasible disassembly sequence of the device, particular of a guided
missile weaponry device, the guided
missile weaponry device is complex in
assembly structure and large in maintenance operation difficulty, wrong disassembly operation and procedure usually lead to damage of the device and danger is brought to an operator. According to disassembly characteristics of the guided missile device, a disassembly
risk factor serves as a cost function, based on the foundation that disassembly safety is considered, a selective disassembly sequence optimized model based on mutual restriction relationship of parts is established, a selective disassembly sequence optimized
algorithm based on an
ant colony
algorithm is designed and the optimal selective disassembly sequence or the selective disassembly sequence close to optimization is searched from all the feasible sequences. The virtual prototype disassembly
sequence planning method can guide practical
assembly and maintenance operation, effectively reduce maintenance and training expense and improve maintenance accuracy and safety.