Zobrazeno 1 - 10
of 88
pro vyhledávání: '"M. Seetharama Bhat"'
Publikováno v:
IEEE Access, Vol 6, Pp 74521-74535 (2018)
The development of a fixed-wing nano air vehicle that fits inside a cube of 75 mm is described in this paper. A novel aircraft configuration that satisfies the static and dynamic stability and the mission performance requirements is developed. A perf
Externí odkaz:
https://doaj.org/article/1bc9e4938c394128aeb4a2b87552e564
Publikováno v:
Micromachines, Vol 9, Iss 3, p 111 (2018)
This paper presents the nonlinear six degrees of freedom dynamic modeling of a fixed wing micro air vehicle. The static derivatives of the micro air vehicle are obtained through the wind tunnel testing. The propeller effects on the lift, drag, pitchi
Externí odkaz:
https://doaj.org/article/63b2a6a65baf4d0d80b8f0bf2a29940c
Autor:
Meenakshi M., M. Seetharama Bhat
Publikováno v:
Journal of Control Science and Engineering, Vol 2011 (2011)
This paper presents the design and development of a fixed low-order, robust H2 controller for a micro air vehicle (MAV) named Sarika-2. The controller synthesis uses strengthened discrete optimal projection equations and frequency-dependent performan
Externí odkaz:
https://doaj.org/article/6c806e2163fb4727a0be78c15113346d
Autor:
Shuvrangshu Jana, Harikumar Kandath, Mayur Shewale, Gunjit Dhingra, Duddela Sai Harish, M. Seetharama Bhat
Publikováno v:
CEAS Aeronautical Journal. 13:433-452
Autor:
Shuvrangshu Jana, Shashank Shivkumar, Mayur Shewale, Harikumar Kandath, Meghana Ramesh, Susheel Balasubramaniam, Eshaan Khanapuri, M. Seetharama Bhat
Publikováno v:
Journal of Aerospace Engineering. 35
Publikováno v:
2021 IEEE 18th India Council International Conference (INDICON).
Autor:
Mayur Shewale, M. Seetharama Bhat, Susheel Balasubramaniam, Harikumar Kandath, Shuvrangshu Jana
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering. 234:677-689
This article presents the implementation of closed-loop simple adaptive control on fixed-wing micro air vehicle dynamics to improve flight performance characteristics. It is known that to retain the micro air vehicle system performance during the ent
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:716-728
This paper presents the analysis of propeller-induced flow effects on the dynamics of a fixed wing biplane micro air vehicle. The analysis is based on wind tunnel tests and mathematical modeling. This analysis plays a pivotal role because the propell
Publikováno v:
Journal of Guidance, Control, and Dynamics. 41:2687-2694
The solution to the simultaneous stabilization problem of a finite set of MIMO unstable plants considered in this Note is based on the frequency-shaped central plant and its sufficiency condition for simultaneous stabilization. The novel method propo
Autor:
M. Seetharama Bhat, Shuvrangshu Jana
Publikováno v:
IFAC-PapersOnLine. 51:178-183
This paper introduces robust estimation of micro air vehicle’s linear velocity from captured images using a monocular camera in GPS denied environment. Vehicle’s velocity information can be extracted from matched feature points of consecutive ima