hesented are results of a study of the application of linear quadratic optimal model-following control applied to a Bell 205 helicopter in hover. The primary objective of good in-flight stability robustness and performance was accomplished via singular value analysis using perturbed systems. Nominal
โฆ LIBER โฆ
Linearization by means of optimal control for a model in plasma physics
โ Scribed by Claudia Lidia Simionescu
- Publisher
- Elsevier Science
- Year
- 1980
- Tongue
- English
- Weight
- 471 KB
- Volume
- 18
- Category
- Article
- ISSN
- 0020-7225
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