Guidance Law Design for Missiles with Reduced Seeker Field-of-View
- Author(s):
- M. Xin ( Mississippi State University, Starkville, MS )
- S. Balakrishnan ( University of Missouri-Rolla, Rolla, MO )
- E. Ohlmeyer ( Naval Surface Weapon Center, Dahlgren, VA )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Guidance Navigation and Control Conference
- Ser. no.:
- 2006
- Pub. Year:
- 2006
- No.:
- 2006-6085
- Paper no.:
- AIAA Paper 2006-6085
- Pub. info.:
- Reston, Va: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200619 [CD-ROM 2006 Disc 19]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
A New Optimal Nonlinear Control Method and its Application to Missile Guidance Law Design
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Nonlinear Bank-to-Turn/Skid-to-Turn Missile Outer-Loop/Inner-Loop Autopilot Design with theta-D Technique
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Reduced order H。?missile controller synthesis using critical characteristic capture
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |