Synthesis of optimal feedback guidance l
โ
N. Rahbar; M. Bahrami
๐
Article
๐
2000
๐
John Wiley and Sons
๐
English
โ 81 KB
๐ 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