Refine your search
Collections
Journals
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z All
Shaw, Vikash
- Geometric Parameters Selection of a Multirole Fighter Aircraft
Abstract Views :274 |
PDF Views:7
Authors
Vikash Shaw
1,
S. K. Samal
1
Affiliations
1 Department of Aeronautical Engineering, Bhubaneswar Engineering College, Bhubaneswar, Odisha, IN
1 Department of Aeronautical Engineering, Bhubaneswar Engineering College, Bhubaneswar, Odisha, IN
Source
Technology Spectrum Review, Vol 2, No 2 (2017), Pagination: 21-24Abstract
Our project is to design a multirole fighter jet aircraft. A multirole fighter jet aircraft is an aircraft designed to perform different roles in warfare. The air-to-air combat role has been normally performed by fighter aircraft. In addition, a multirole fighter jet aircraft has secondary roles such as air-to-surface attack, intercepting, reconnaissance, escorting and air cover. The term multirole has been reserved for aircraft designed with the aim of using a common airframe for multiple tasks where the same basic airframe is adapted to a number of differing roles. The main motivation for developing multirole aircraft is cost reduction in using a common airframe. The project report comprises of a literature survey of about 10 fighter aircrafts. After this an appropriate aerofoil is selected and its important parameters are computed. Then, performance graphs are drawn and a 3-view diagram of the aircraft is drawn. Finally, model is made and tested.Keywords
Fighter, Multirole, Span, Thrust to Weight.
References
- R. T. Whitcomb, “Methods for reducing subsonic drag due to lift,” Special course on concepts for drag reduction, AGARD, France, pp. 2-1 to 2-11, 1977.
- https://pix4d.com/industry/agricultur/
- https://pix4d.com/industry/real-estate/
- R. Graham, and R. Read, Manual Aerial Survey, Whittles Publishing, 2002.
- J. M. Wu, A. Vakili, and Z. L. Chen, “Wing tip jets aerodynamics performance,” 13th Congress of the International Council of the Aeronautical Sciences/AIAA Aircraft Systems and Technology Conference, ICAS Proceedings, vol. 2, pp. 1115-1121, 1982.
- H. Zimmer, “The aerodynamic optimization of wings at subsonic speeds and the influence of wingtip design,” NASA TM-88534, 1983.
- The Flying Wing UAV Using Classical Control Theory
Abstract Views :468 |
PDF Views:0
Authors
Affiliations
1 Bhubaneswar Engineering College, Bhubaneswar, Odisha, IN
1 Bhubaneswar Engineering College, Bhubaneswar, Odisha, IN
Source
Technology Spectrum Review, Vol 3, No 1&2 (2018), Pagination: 1-4Abstract
This paper describes modeling design procedure of a flying wing UAV which is a tailless fixed wing aircraft and has no definite fuselage, with respect of the crew, payload and equipment being housed inside the main wing structure. In this thesis a 6 degree-of-freedom mathematical model describing the aircraft dynamics is first presented, then using these equations, the derivatives of the parameters and system identification of simplified, linear lateral and longitudinal models are estimated for the tailless aircraft. A detailed modeling procedure of flying wing UAV and stability analysis results using the linearized model at trim condition are represented. Finally, we have designed the flying wing UAV using classical control theory.Keywords
Control, Designe, Model, UAV.References
- O. I. Elgerd, Electric Energy Systems Theory: An Introduction, Tata McGraw-Hill, New Delhi, 1983.
- O. I. Elgerd, Electric Energy Systems Theory: An Introduction, McGraw Hill Co., 2001.
- O. I. Elgerd, and C. E. Fosha, “Optimum megawatt-frequency control of multiarea electric energy systems,” IEEE Transactons on Power Apparatus and Systems, vol. PAS-89, no. 4, pp. 556-563, April 1970.
- D. Rerkpreedapong, A. Hasanovic, and A. Feliachi, “Robust load frequency control using genetic algorithms and linear matrix inequalities,” IEEE Transactions on Power Systems, vol. 18, no. 2, pp. 855-861, 2003.
- T. C. Yang, H. Cimen, and Q. M. Zhu, “Decentralized load-frequency controller design based on structured singular values,” IEE Proceedings - Generation, Transmission and Distribution, vol. 145, no. 1, pp. 7-14, 1998.
- P. Kundur, Power System Stability and Control, Mc-Grall Hill, New York, 1994.
- S. P. Ghosal, “Multi-area frequency and tie-line power flow control with fuzzy logic based integral gain scheduling,” Journal of the Institution of Engineers (India): Electrical Engineering Division, vol. 84, no. 3, pp. 135-141, 2003.
- S. P. Ghosal, “Application of GA/GA-SA based fuzzy automatic generation control of a multi-area thermal generating system,” Elec. Pow. Sys. Res., vol. 70, no. 2, pp. 115-127, July 2004.
- M. L. Kothari, J. Nanda, D. P. Kothari, and D. Das, “Discrete-mode automatic generation control of a two-area reheat thermal system with new area control error,” IEEE Transactions on Power Systems, vol. 4, no. 2, pp. 730-738, May 1989.
- K. Venkateswarlu, and A. K. Mahalanabis, “Load frequency control using output feedback,” Journal of the Institution of Engineers (India), pt. El-4, vol. 58, pp. 200-203, February 1978.
- S. Pothiya, I. Ngamroo, S. Runggeratigul, and P. Tantaswadi, “Design of optimal fuzzy logic based PI controller using multiple tabu search algorithms for load frequency control,” International Journal of Control, Automation and Systems, vol. 4, no. 2, pp. 155-164, April 2006.
- M. L. Kothari, J. Nanda, D. P. Kothari, and D. Das, “Discrete-mode automatic generation control of a two-area reheat thermal system with new area control error,” IEEE Transactions on Power Systems, vol. 4, no. 2, pp. 730-738, June 1989.
- D. K. Chaturvedi, P. S. Satsangi, and P. K. Kalra, “Load frequency control: A generalized neural network approach,” International Journal of Electrical Power & Energy Systems, vol. 21, no. 6, pp. 405- 415, 1999.
- E. Cam, and I. Kocaarslan, “Fuzzy logic controller in interconnected electrical power systems for load-frequency control,” International Journal of Electrical Power & Energy Systems, vol. 27, no. 8, pp. 542-549, 2005.