to implement a generic fighter aircraft one dimensional longitudinal flight controls (pitch mode) using simulation techniques and implement it physically so as to simulate various flight stability charactertics and dynamic properties of the aircraft G-62
Publisher: Risalpur NUST 2007Description: ix, 99 pDDC classification: PR 380| Item type | Current location | Home library | Collection | Call number | Status | Date due | Barcode | Item holds |
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Book
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College of Aeronautical Engineering (CAE) | College of Aeronautical Engineering (CAE) | NFIC | PR 380 (Browse shelf) | Available | CAEPR-380 |
Total holds: 0
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