Design of the dynamic analyse system for missile pilot stabilized loop
Su An
Abstract
Su An
Abstract
For researching parameters of missile stabilized loop to performance effect of missile control system,a dynamic analyse sys-tem for missile pilot stabilized loop is devised. The system uses a industrial control computer as a core,the A/D、D/A、and time arithmometer boards are assembled as a cascade structure. Using automatic test hardware facility and increasing software and hardware anti-jamming measures,it improves test precision. Test result indicates that the system can be applied well in the test parameter analyse of the pilot stabilized loop,and has good theory value and practical significance.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
For researching parameters of missile stabilized loop to performance effect of missile control system,a dynamic analyse sys-tem for missile pilot stabilized loop is devised. The system uses a industrial control computer as a core,the A/D、D/A、and time arithmometer boards are assembled as a cascade structure. Using automatic test hardware facility and increasing software and hardware anti-jamming measures,it improves test precision. Test result indicates that the system can be applied well in the test parameter analyse of the pilot stabilized loop,and has good theory value and practical significance.
Key concepts: Missile, Computer science, Hardware-in-the-loop simulation, Cascade, Loop (graph theory), Software, Simulation, Missile guidance