Open loop and closed loop analysis of fixed wing micro aerial vehicle for impulsive launch techniqiues (R)
Material type:![Text](/opac-tmpl/lib/famfamfam/BK.png)
Item type | Current library | Call number | Status | Date due | Barcode | Item holds |
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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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