Open loop and closed loop analysis of fixed wing micro aerial vehicle for impulsive launch techniqiues (R)
Material type:
TextLanguage: English Publication details: Mumbai IIT 2019Description: xx,130 p. 30 cmSubject(s): Theses and Dissertations | Flight control | Control theory | Micro air vehicles | Launch vehicles | Mathematical optimization | Aerospace engineeringDissertation note: Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aerospace Engineering 2019
| Item type | Current library | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|
Theses and Dissertations
|
Central Library, IITB Pamphlet Section (Theses, Standards, Reports) | 043:629.13.014.5 Bal | Not for loan | 246147 |
Total holds: 0
Thesis Ph.D. Indian Institute of Technology Bombay. Department of Aerospace Engineering 2019
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