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ORCIDKrishna Dev Kumar
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2020 – today
- 2024
[i1]Siavash Tavana, Sepideh Faghihi, Anton H. J. de Ruiter, Krishna Dev Kumar:
A Novel Optimization-Based Collision Avoidance For Autonomous On-Orbit Assembly. CoRR abs/2404.07916 (2024)- 2023
- [j25]Kaustav Jyoti Borah
, Krishna Dev Kumar:
Consensus Tracking of Multi-Agent Systems in Presence of Uncertain Dynamics and Communications Faults. IEEE Access 11: 120304-120318 (2023) - [j24]Rui Qi, Yang Zhang, Krishna Dev Kumar:
Design and Robustness Analysis of a Wave-Based Controller for Tethered Towing of Defunct Satellites. IEEE CAA J. Autom. Sinica 10(1): 278-280 (2023) - 2021
- [c5]Unit Amin, Krishna Dev Kumar:
Remaining Useful Life Prediction of Aircraft Engines Using Hybrid Model Based on Artificial Intelligence Techniques. ICPHM 2021: 1-10 - 2020
- [j23]An-Min Zou, Krishna Dev Kumar, Anton H. J. de Ruiter:
Fixed-time attitude tracking control for rigid spacecraft. Autom. 113: 108792 (2020) - [j22]Afshin Rahimi, Krishna Dev Kumar, Hekmat Alighanbari:
Fault Isolation of Reaction Wheels for Satellite Attitude Control. IEEE Trans. Aerosp. Electron. Syst. 56(1): 610-629 (2020) - [j21]Chengfei Yue, Fan Wu, Feng Wang, Xibin Cao, Qiang Shen, Krishna Dev Kumar:
Two Parallel Single-Gimbal Control Moment Gyros Actuated Spacecraft Attitude Maneuver. IEEE Trans. Aerosp. Electron. Syst. 56(5): 4112-4123 (2020)
2010 – 2019
- 2019
- [j20]An-Min Zou, Anton H. J. de Ruiter, Krishna Dev Kumar:
Comments on "Adaptive tracking control of uncertain MIMO nonlinear systems with input constraints". Autom. 100: 417-418 (2019) - [j19]Alexander Frias, Anton H. J. de Ruiter, Krishna Dev Kumar:
Velocity-free spacecraft attitude stabilization using two control torques. Autom. 109 (2019) - [j18]An-Min Zou, Anton H. J. de Ruiter, Krishna Dev Kumar:
Disturbance Observer-Based Attitude Control for Spacecraft With Input MRS. IEEE Trans. Aerosp. Electron. Syst. 55(1): 384-396 (2019) - 2017
- [j17]An-Min Zou, Krishna Dev Kumar, Anton H. J. de Ruiter:
Spacecraft attitude control using two control torques. Inf. Sci. 408: 23-40 (2017) - 2016
- [j16]An-Min Zou, Anton H. J. de Ruiter, Krishna Dev Kumar:
Distributed finite-time velocity-free attitude coordination control for spacecraft formations. Autom. 67: 46-53 (2016) - [j15]An-Min Zou, Anton H. J. de Ruiter, Krishna Dev Kumar:
Distributed attitude synchronization control for a group of flexible spacecraft using only attitude measurements. Inf. Sci. 343-344: 66-78 (2016) - [j14]An-Min Zou, Anton H. J. de Ruiter, Krishna Dev Kumar:
Finite-time output feedback attitude control for rigid spacecraft under control input saturation. J. Frankl. Inst. 353(17): 4442-4470 (2016) - 2015
- [j13]Afshin Rahimi, Krishna Dev Kumar, Hekmat Alighanbari:
Enhanced adaptive unscented Kalman filter for reaction wheels. IEEE Trans. Aerosp. Electron. Syst. 51(2): 1568-1575 (2015) - 2013
- [j12]An-Min Zou, Krishna Dev Kumar, Zeng-Guang Hou:
Correction to "Attitude Coordination Control for a Group of Spacecraft Without Velocity Measurements". IEEE Trans. Control. Syst. Technol. 21(3): 1044 (2013) - [j11]An-Min Zou, Krishna Dev Kumar, Zeng-Guang Hou:
Corrections to "Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Model and Chebyshev Neural Network". IEEE Trans. Cybern. 43(2): 803 (2013) - [c4]Afshin Rahimi, Kaamran Raahemifar, Krishna Dev Kumar, Hekmat Alighanbari:
Controller design for rotary inverted pendulum system using particle swarm optimization algorithm. CCECE 2013: 1-5 - 2012
- [j10]Yaodong Pan, Krishna Dev Kumar, Guangjun Liu:
Extremum Seeking Control with Second-Order Sliding Mode. SIAM J. Control. Optim. 50(6): 3292-3309 (2012) - [j9]An-Min Zou, Krishna Dev Kumar:
Distributed Attitude Coordination Control for Spacecraft Formation Flying. IEEE Trans. Aerosp. Electron. Syst. 48(2): 1329-1346 (2012) - [j8]Xi Liu, Krishna Dev Kumar:
Network-Based Tracking Control of Spacecraft Formation Flying with Communication Delays. IEEE Trans. Aerosp. Electron. Syst. 48(3): 2302-2314 (2012) - [j7]An-Min Zou, Krishna Dev Kumar, Zeng-Guang Hou:
Attitude Coordination Control for a Group of Spacecraft Without Velocity Measurements. IEEE Trans. Control. Syst. Technol. 20(5): 1160-1174 (2012) - [j6]Junquan Li, Krishna Dev Kumar:
Decentralized Fault-Tolerant Control for Satellite Attitude Synchronization. IEEE Trans. Fuzzy Syst. 20(3): 572-586 (2012) - [j5]An-Min Zou, Krishna Dev Kumar:
Neural Network-Based Distributed Attitude Coordination Control for Spacecraft Formation Flying With Input Saturation. IEEE Trans. Neural Networks Learn. Syst. 23(7): 1155-1162 (2012) - 2011
- [j4]An-Min Zou, Krishna Dev Kumar, Zeng-Guang Hou, Xi Liu:
Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Mode and Chebyshev Neural Network. IEEE Trans. Syst. Man Cybern. Part B 41(4): 950-963 (2011) - [c3]Junquan Li, Krishna Dev Kumar:
Decentralized fuzzy fault tolerant control for multiple satellites attitude synchronization. FUZZ-IEEE 2011: 1836-1843 - [c2]Junquan Li, Krishna Dev Kumar:
Intelligent Fault Detection, Identification and Control of Satellite Formation Flying. ICINCO (1) 2011: 85-90 - 2010
- [j3]An-Min Zou, Krishna Dev Kumar, Zeng-Guang Hou:
Quaternion-based adaptive output feedback attitude control of spacecraft using Chebyshev neural networks. IEEE Trans. Neural Networks 21(9): 1457-1471 (2010) - [c1]Xi Liu, Krishna Dev Kumar:
Formation control of spacecraft flying with network-induced delays and packet dropouts. ICCA 2010: 480-485
2000 – 2009
- 2009
- [j2]Yaodong Pan, Krishna Dev Kumar, Guangjun Liu, Katsuhisa Furuta:
Design of Variable Structure Control System With Nonlinear Time-Varying Sliding Sector. IEEE Trans. Autom. Control. 54(8): 1981-1986 (2009) - 2008
- [j1]M. W. R. Alger, Krishna Dev Kumar:
A design and development of Pico- and Femto-satellites. Int. J. Manuf. Res. 3(1): 48-79 (2008)
Coauthor Index
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