New PDF release: A-6 Intruder

By Lou Drendel:

;A-6 Intruder [Modern army airplane sequence 5007] КНИГИ ;ВОЕННАЯ ИСТОРИЯ Автор: Lou Drendel: Название: A-6 Intruder [Modern army plane sequence 5007]:Серия: glossy army plane sequence 5007:Издательство: Squadron/Signal publications:Страниц: 64:Язык: Английский:Год: 1991:Формат: pdf в rar:Размер: 77,3 Mb:Для сайта: www.mirknig.comОписание (About this book): The Grumman A-6 Intruder is a dual jet-engine, mid-wing assault airplane outfitted by means of Grumman Aerospace. In provider among 1963 and 1997, the Intruder used to be designed as an all-weather substitute for the piston-engined A-1 Skyraider medium assault airplane. A really good digital struggle spinoff, the EA-6B Prowler, continues to be in carrier as of 2009. because the A-6 used to be slated for retirement, its precision strike venture used to be taken over via the now retired F-14 Tomcat built with LANTIRN pod. eighty five

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R. Napolitano et al. / Aircraft Design 4 (2001) 19}50 [25] Hoak DE, Finck RD. USAF stability and control DATCOM. AFWAL-TR-83-3048, October 1960, Revised 1978. [26] Patcher M, Chandler PR, Nelson E, Rasmussen S. Parameter estimation for over-actuated aircraft with non linear aerodynamics. Proceedings of the 1999 AIAA Guidance Navigation and Control Conference, AIAA Paper 99-4046, Portland, OR, August 1999. [27] Bu$ngton J, Chandler PR, Patcher M. Integration of on-line system identi"cation and optimization-based control allocation.

Proceedings of the 1999 American Control Conference, San Diego, CA, June 1999. [8] Rysdyk R, Calise, AJ. Fault tolerant #ight control via adaptive neural network augmentation. Proceedings of the 1998 AIAA Guidance Navigation and Control Conference, AIAA Paper 98-4483, Boston, MA, August 1998. [9] Napolitano MR, Chen CI, Naylor S. Aircraft failure detection and identi"cation using neural networks. AIAA Journal of Guidance, Control and Dynamics 1993;16(6):999}1009. [10] Napolitano MR, Younghwan A, Seanor B.

Proceedings of the 1998 AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 98-4261, Boston, MA, August 1998. [22] Morelli EA. High accuracy evaluation of the "nite Fourier transform using sampled data. NASA TM 110340, June 1997. [23] Klein V. Aircraft parameter estimation in frequency domain. Proceedings of the 1978 AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 78-1344, Palo Alto, CA, August 1978. [24] Roskam J. Airplane #ight dynamics and automatic #ight controls: Part I. Roskam Aviation and Engineering Coorporation, Ottawa, KA, 1994.

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