𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Near-Optimal Guidance Law for Ballistic Missile Interception

✍ Scribed by Dougherty, John J.; Speyer, Jason L.


Book ID
120169786
Publisher
American Institute of Aeronautics and Astronautics
Year
1997
Tongue
English
Weight
361 KB
Volume
20
Category
Article
ISSN
0731-5090

No coin nor oath required. For personal study only.


πŸ“œ SIMILAR VOLUMES


An All-Aspect Near-Optimal Guidance Law
✍ Y. C. Sim; S. B. Leng; V. Subramaniam πŸ“‚ Article πŸ“… 2000 πŸ› Springer 🌐 English βš– 251 KB
Synthesis of optimal feedback guidance l
✍ N. Rahbar; M. Bahrami πŸ“‚ Article πŸ“… 2000 πŸ› John Wiley and Sons 🌐 English βš– 81 KB πŸ‘ 1 views

Most existing missiles are guided by proportional navigation guidance (PNG) law, but PNG is a particular case for LQ guidance rule with two main assumptions of small line-of-sight angles and negligible acceleration along the line-of-sight. However, most missile engagements exceed these limits becaus