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Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2016) 88 (6): 689–696.
Published: 03 October 2016
... with respect to the c.g. of the aircraft. The engine thrust T, lift L, drag D and pitch moment M are given by: (2) r c = r c0 + 1 2 r ¨ c t 2 Airdrop Feedback linearization Flight control Low altitude Nonlinear integral...

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