TY - GEN
T1 - Guidance and Control System Making Use of Low Cost IMU/GPS for Guided Artillery Rocket
AU - She, Haoping
AU - Yang, Shuxing
PY - 2003
Y1 - 2003
N2 - To improve accuracy of artillery rocket is a crucial problem especially for long-range multiple launch rocket system. A kind of simplified control system can control the rocket during boost phase, but cannot compensate for disturbance during coast phase. In this paper, a guidance and control system making use of low cost IMU/GPS (Inertial Measurement Unit/Global Positioning System) is introduced, by which disturbance during both phase can be restricted. Guidance adds extra cost to the rocket but is more than offset by increased effectiveness.
AB - To improve accuracy of artillery rocket is a crucial problem especially for long-range multiple launch rocket system. A kind of simplified control system can control the rocket during boost phase, but cannot compensate for disturbance during coast phase. In this paper, a guidance and control system making use of low cost IMU/GPS (Inertial Measurement Unit/Global Positioning System) is introduced, by which disturbance during both phase can be restricted. Guidance adds extra cost to the rocket but is more than offset by increased effectiveness.
KW - Artillery Rocket
KW - Global Positioning System (GPS)
KW - Guidance and control system
KW - Inertial Navigation System (INS)
UR - http://www.scopus.com/inward/record.url?scp=0141425570&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:0141425570
T3 - Proceedings of the International Symposium on Test and Measurement
SP - 93
EP - 95
BT - Proceedings of the International Symposium on Test and Measurement
ER -