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Computational optimal control of the terminal bunt manoeuvre—Part 2: minimum-time case

✍ Scribed by S. Subchan; R. Żbikowski


Publisher
John Wiley and Sons
Year
2007
Tongue
English
Weight
527 KB
Volume
28
Category
Article
ISSN
0143-2087

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Computational optimal control of the ter
✍ S. Subchan; R. Zbikowski 📂 Article 📅 2007 🏛 John Wiley and Sons 🌐 English ⚖ 784 KB

## Abstract This two‐part paper studies trajectory shaping of a generic cruise missile attacking a fixed target from above. This guidance problem is reinterpreted using optimal control theory resulting in two formulations: (1) minimum time‐integrated altitude (part 1) and (2) minimum flight time (p