Evaluation of Two Guidance Laws for Controlling the Impact Flight Path Angle of a Naval Gun Launched Spinning Projectile
- Author(s):
- K. Pamadi ( Naval Surface Warfare Center, Dahlren, VA )
- E. Ohlmeyer
- 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.:
- 2006-6081
- Paper no.:
- AIAA Paper 2006-6081
- 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:
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 |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Robust Guidance and Control Algorithms Using Constant Flight Path Angle for Precision Landing on Mars
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |