TY - GEN
T1 - The design of the height navigation system of target missile
AU - Hai, Wang
AU - Li, Sun
AU - Jie, Yan
PY - 2009
Y1 - 2009
N2 - For the need of some kind of target missile, this paper proposes a method to design a height navigation system, which is composed of MOTOROLA MPX2100 pressure sensor, MCU and XW-IMU5200 inertial navigation chip. Based on the analysis of the inertial navigation system error, atmospheric pressure height model and atmospheric data, a hardware system has been designed according to the flight height range of the target missile and the algorithm of the navigation system has been improved. The result shows that the new navigation system has high precision and reliability property. For the need of some kind of target missile, this paper proposes a method to design a height navigation system, which is composed of MOTOROLA MPX2100 pressure sensor, MCU and XW-IMU5200 inertial navigation chip. Based on the analysis of the inertial navigation system error, atmospheric pressure height model and atmospheric data, a hardware system has been designed according to the flight height range of the target missile and the algorithm of the navigation system has been improved. The result shows that the new navigation system has high precision and reliability property.
AB - For the need of some kind of target missile, this paper proposes a method to design a height navigation system, which is composed of MOTOROLA MPX2100 pressure sensor, MCU and XW-IMU5200 inertial navigation chip. Based on the analysis of the inertial navigation system error, atmospheric pressure height model and atmospheric data, a hardware system has been designed according to the flight height range of the target missile and the algorithm of the navigation system has been improved. The result shows that the new navigation system has high precision and reliability property. For the need of some kind of target missile, this paper proposes a method to design a height navigation system, which is composed of MOTOROLA MPX2100 pressure sensor, MCU and XW-IMU5200 inertial navigation chip. Based on the analysis of the inertial navigation system error, atmospheric pressure height model and atmospheric data, a hardware system has been designed according to the flight height range of the target missile and the algorithm of the navigation system has been improved. The result shows that the new navigation system has high precision and reliability property.
KW - Atmospheric data
KW - Filter
KW - Integrated navigation system
KW - Pressure sensor
UR - https://www.scopus.com/pages/publications/71549158230
U2 - 10.1109/ICEMI.2009.5274351
DO - 10.1109/ICEMI.2009.5274351
M3 - 会议稿件
AN - SCOPUS:71549158230
SN - 9781424438624
T3 - ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments
SP - 3142
EP - 3145
BT - ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments
T2 - 9th International Conference on Electronic Measurement and Instruments, ICEMI 2009
Y2 - 16 August 2009 through 19 August 2009
ER -