1Mario Innocenti & Ajay Thukral.Simultaneous reaction jet and aerodynamic control of missile systems[R].AIAA-93-3739-CP
2Rui Hirokawa,el.Autopilot design for a missile with reaction jet using coefficient diagram method[C].Montreal,Canada,AIAA Guidance,Navigation,and Control Conference and Exhibit,August 2001
3Lin T C,Sproul L K,Mckeel S A,et al..Novel approach for maneuvering reentry vehicle design[J].Journal of Spacecraft and Rockets,2003,40(5):605-614
4Fote P & Thyson N A.Conventional ballistic missile design manual[R].Textron System Div.,Rept,TSC-272-100047,Wilmington,MA,May 1999
5Ping Lu,Zuojun Shen.Control of nonlinear systems with two time scales[R].AIAA 2001-4166
6Innocenti M, ThukraI A. Simultaneous reaction jet and aerodynamic control of missile systems[R]. AIAA-93-3739-CP, 1993.
7Hirokawa R. Autopilot design for a missile with reaction jet using coefficient diagram method[J]. Montreal,Canada .AIAA Guidance. Navigation ,and Control Conference and Exhibit , 2001.
8Lin T C, SprouI L K, Mckeel S A,et al. Novel approach for maneuvering reentry vehicle design[J]. Journal of Spacecraft and Rockets, 2003,40(5): 605 - 614.
1Mario Innocenti & Ajay Thukral.Simultaneous reaction jet and aerodynamic control of missile systems[R].AIAA-93-3739-CP
2Rui Hirokawa,el.Autopilot design for a missile with reaction jet using coefficient diagram method[C].Montreal,Canada,AIAA Guidance,Navigation,and Control Conference and Exhibit,August 2001
3Lin T C,Sproul L K,Mckeel S A,et al..Novel approach for maneuvering reentry vehicle design[J].Journal of Spacecraft and Rockets,2003,40(5):605-614
4Fote P & Thyson N A.Conventional ballistic missile design manual[R].Textron System Div.,Rept,TSC-272-100047,Wilmington,MA,May 1999
5Ping Lu,Zuojun Shen.Control of nonlinear systems with two time scales[R].AIAA 2001-4166
6Innocenti M, ThukraI A. Simultaneous reaction jet and aerodynamic control of missile systems[R]. AIAA-93-3739-CP, 1993.
7Hirokawa R. Autopilot design for a missile with reaction jet using coefficient diagram method[J]. Montreal,Canada .AIAA Guidance. Navigation ,and Control Conference and Exhibit , 2001.
8Lin T C, SprouI L K, Mckeel S A,et al. Novel approach for maneuvering reentry vehicle design[J]. Journal of Spacecraft and Rockets, 2003,40(5): 605 - 614.
