Zobrazeno 1 - 10
of 15
pro vyhledávání: '"N Shantha Kumar"'
Analysis of A Regenerative Braking System of BLDC Motor In Targeting Electric Vehicle Implementation
Autor:
Umesh Kumar Singh, N. Shantha Kumar
Publikováno v:
2022 Fourth International Conference on Emerging Research in Electronics, Computer Science and Technology (ICERECT).
Autor:
N. Shantha Kumar, Alka Verma
Publikováno v:
2022 Second International Conference on Advanced Technologies in Intelligent Control, Environment, Computing & Communication Engineering (ICATIECE).
Autor:
N. Shantha Kumar, Deepak Kumar Sinha
Publikováno v:
2022 11th International Conference on System Modeling & Advancement in Research Trends (SMART).
Autor:
P N Shantha Kumar, Narendra Kumar L
Publikováno v:
MedPulse International Journal of Surgery. 9:164-167
Autor:
Narendra Kumar L, P N Shantha Kumar
Publikováno v:
MedPulse International Journal of Surgery. 10:18-20
Autor:
N Shantha Kumar, N Aishwarya, Sudesh K. Kashyap, Sanketh Ailneni, D David Livingstone, K V Karthik, Neenu Varghese
Publikováno v:
2019 International Conference on Range Technology (ICORT).
Inertial system consisting of 10 DoF MEMS IMU has been brought to deploy on the stores of high performance fighter aircraft to estimate the separation trajectory of released stores from the aircraft. The IMU calibration has been carried out as it is
Publikováno v:
International Journal of Intelligent Unmanned Systems. 2:154-167
Purpose– The purpose of this paper is to present fusion of inertial navigation system (INS) and global positioning system (GPS) for estimating position, velocities, attitude and heading of an unmanned aerial vehicle (UAV).Design/methodology/approac
Publikováno v:
ASCC
Novel sensor fusion architecture is proposed to provide complete navigational solution for micro aerial vehicles (MAV) using low cost sensors and micro controller. The approach uses a nonlinear complementary filter (NCF) to estimate direction cosine
Autor:
N. Janardhana Rao, N Shantha Kumar
Publikováno v:
Defence Science Journal. 54:277-292
In this paper, stability and control derivatives of light canard research aircraft generated through the flight test using parameter estimation technique has been presented. The maximum likelihood estimation, based on output-error minimisation techni
Autor:
N Shantha Kumar, T. Jann
Publikováno v:
Sadhana. 29:217-235
Due to costs, size and mass, commercially available inertial navigation systems are not suitable for small, autonomous flying vehicles like ALEX and other UAVs. In contrast, by using modern MEMS (or of similar class) sensors, hardware costs, size and