Research on four-dimensional guidance and control for missile cooperative engagementChinese Full Text
CUI Nai-gang,WEI Chang-zhu,GUO Ji-feng(Department of Astronautic Engineering,Harbin Institute of Technology,Harbin 150001,China)
Abstract: This paper proposed a control framework of four-dimensional guidance for the cooperative engagement of missile with three profiles.Taking a missile with BTT control mode as an example,research on the control method of four-dimensional guidance was conducted.The velocity/altitude decoupling controller suitable for the BTT missile with overload autopilot inner-loop was designed based on total energy control theory analysis,which implemented the decoupling for velocity and altitude profiles in four-dimensional guidance control framework.In the end,simulation verification was performed to show that the four-dimensional guidance controller is able to implement the cooperative engagement by controlling a missile according to instructions of the task planning system.
Keywords：
four-dimensional guidance; cooperative engagement; total energy control; decoupling; inner-loop;
- DOI：
10.13645/j.cnki.f.d.2010.02.023
- Series：
- Subject：
- Classification Code：
TJ765.3
- Mobile Reading
Read on your phone instantly
Step 1Scan QR Codes
"Mobile CNKI-CNKI Express" App
Step 2Open“CNKI Express”
and click the scan icon in the upper left corner of the homepage.
Step 3
Scan QR Codes
Read this article on your phone.
- HTML
- CAJ Download
- PDF Download
Download the mobile appuse the app to scan this coderead the article.
Tips: Please download CAJViewer to view CAJ format full text.
Download: 544 Page: 63-66 Pagecount: 4 Size: 376K
Citation Network
Related Literature
- Similar Article
- Reader Recommendation
- Associated Author