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Nandan K. Sinha
Researcher at Indian Institute of Technology Madras
Publications - 53
Citations - 446
Nandan K. Sinha is an academic researcher from Indian Institute of Technology Madras. The author has contributed to research in topics: Nonlinear system & Flight dynamics. The author has an hindex of 10, co-authored 48 publications receiving 395 citations. Previous affiliations of Nandan K. Sinha include Technische Universität Darmstadt & Indian Institutes of Technology.
Papers
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Journal ArticleDOI
Level Flight Trim and Stability Analysis Using Extended Bifurcation and Continuation Procedure
TL;DR: Hollkamp et al. as mentioned in this paper proposed a self-tuning piezoelectric Vibration Absorber for passive vibration suppression in wing-like composite structures.
Proceedings ArticleDOI
Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis - A State-of-the-Art
TL;DR: The state-of-the-art in the use of bifurcation and continuation methods for the analysis of aircraft trim and stability with a few illustrative examples are described.
Journal ArticleDOI
Aircraft Maneuver Design Using Bifurcation Analysis and Sliding Mode Control Techniques
TL;DR: In this article, bifurcation analysis-based methodology is used in conjunction with a sliding-mode-based control algorithm to construct and simulate maneuvers for a nonlinear, 6 degree-of-freedom, F-18 high-alpha research vehicle aircraft model.
Journal ArticleDOI
A New Guidance Law for the Defense Missile of Nonmaneuverable Aircraft
TL;DR: The results show that the performances of COIP and A-CLOS guidance laws are almost identical in a coplanar engagement scenario, but the COIP law has the additional advantage of working with only position information, without the knowledge of motion of the players.
Journal ArticleDOI
Aircraft Spin Recovery Using a Sliding-Mode Controller
TL;DR: In this article, a sliding-mode (SM) controller based on variable-structure control technique for spin recovery of aircraft is presented. But, the controller is not suitable for high-angle-of-attack flight regimes.