Aerospace Engineering

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Journal
• Satellite Attitude Control using Double-Gimbal Variable-Speed Control Moment Gyro: Single-Loop Control Formulation, Sinha M., Barman S. By AIAA Journal of Guidance Control and Dynamics yy 00-00 (2023)
• Singularity Avoidance Controller Design for Spacecraft Attitude Control using Double-Gimbal Variable-Speed Control Moment Gyro Barman S., Sinha M. By European Journal of Control 70 1-14 (2023)
• Satellite Attitude Control using Double-Gimbal Variable-Speed Control Moment Gyro with Unbalanced Rotor Barman S., Sinha M. By AIAA Journal of Guidance Control and Dynamics 46 00-00 (2022)
• Unwinding-Free Fast Finite-Time Sliding Mode Satellite Attitude Tracking Control Das G., Sinha M. By AIAA Journal of Guidance Control and Dynamics 46 1-18 (2022)
• Fault-tolerant sliding mode satellite attitude stabilization using magneto-Coulombic torquers Prabhat H., Mukherjee B.K., Giri D.K., Sinha M. By Aerospace Science and Technology 121 - (2022)
• Automatic control of an asymmetric fighter aircraft performing supermanoeuvres Mukherjee B.K., Goel K., Sinha M. By Advances in Military Technology 15 163-178 (2020)
• Robust backstepping magnetic attitude control of satellite subject to unsymmetrical mass properties Giri D.K., Sinha M. By Journal of Spacecraft and Rockets 56 298-305 (2019)
• Fast terminal sliding-mode fault-tolerant attitude control of magnetically actuated satellite Giri D.K., Sinha M. By Journal of Spacecraft and Rockets 56 1636-1645 (2019)
• ast-terminal Sliding Mode Fault-tolerant Attitude Control ofMagnetically Actuated Satellit Giri D. K., Sinha M. By AIAA Journal of Spacecraft and Rockets 56 1-10 (2019)
• Nonlinear dynamics and control of a laterally mass varying fighter aircraft Mukherjee B.K., Sinha M. By Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232 3118-3134 (2018)
• Fault-tolerant attitude control of miniature satellites using reaction wheels Kumar K.D., Godard, Abreu N., Sinha M. By Acta Astronautica 151 206-216 (2018)
• Finite-time Continuous Sliding Mode Magneto-Coulombic Satellite Attitude Control Giri, D. K. and Sinha, M. By IEEE Transactions of Aerospace Electronic Systems accepted - (2016)
• Fault-Tolerant Attitude Control of Magneto-Coulombic Satellites Giri, D. K., Sinha, M., and Kumar, K. D. By Acta Astronautica 116, 254-270 (2015)
• Fault Detection and Recovery of Spacecraft Formation Flying Using Nonlinear Observer and Reconfigurable Controller Lee, D., Kumar, K. D., and Sinha, M. By Acta Astronautica accepted - (2013)
• Nonlinear and Linear Unstable Aircraft Parameter Estimation Using Neural Partial Differentiation M. Sinha, R. A. Kuttieri, S. Chatterjee By AIAA Journal of Guidance Control and Dynamics accepted - (2013)
• High Angle of Attack Parameter Estimation of Cascaded Fins Using Neural Network M. Sinha, R. A. Kuttieri, A. K. Ghosh, A. Misra By AIAA Journal of Aircraft 55 (1), 272-291 (2013)
• Magneto-Coulombic Attitude Control of Earth Pointing Satellites Giri, D. K. and Sinha, M. By AIAA Journal of Guidance Control and Dynamics accepted - (2013)
• Dynamic Neural Units for Adaptive Magnetic Attitude Control of Spacecrafts Das, S., Sinha, M., Misra, A By AIAA Journal of Guidance Control and Dynamics accepted - (2011)
• Reconfigurable Magnetic Attitude Control of Earth Pointing Satellite Das, S., Sinha, M., Kumar, K. D., Misra, A. By Journal of Aerospace Engineering - (2010)
• Lunar Gravity Field Modeling Critical analysis and challenges Sinha, M., Gopinath, N. S., & Malik N. K. By Advances in Space Research 45 322-249 (2010)
• Neural Network Based Partial Differential Method to Extract Aerodynamic Derivatives from Flight Data Das, S., Kuttieri, R. A., Sinha, M., and, Jategaonkar, R. V. By AIAA Journal of Guidance Control and Dynamics 33 (2) - (2010)
Conferences
• High Precision Satellite Attitude Control using Double-Gimbal Variable-Speed Control Moment Gyro with Unbalanced Rotor Barman S., Sinha M. By Proceedings of the International Astronautical Congress, IAC C1 - (2021)
• Unwinding and Singularity Free Satellite Attitude Control using Double-Gimbal Variable-Speed Control Moment Gyro and Sliding Control Das G., Sinha M. By Proceedings of the International Astronautical Congress, IAC C1 - (2021)
• A Single Loop Dynamic Inversion Control for a Fighter Aircraft Executing Rapid Large Amplitude Maneuvers Mukherjee B.K., Sinha M. By 2017 14th IEEE India Council International Conference, INDICON 2017 - (2018)
• Large angle maneuvering with an asymmetric aircraft: A single loop control formulation Mukherjee B.K., Sinha M. By AIAA Guidance, Navigation, and Control Conference, 2018 - (2018)

Principal Investigator

• LUNAR GRAVITY MODEL AND TOPOGRAPHY DETERMINATION USING GROUND BASED OBSERVATIONS AND LASER ALTIMETRY DATA
• INTELLIGENT FLIGHT CONTROLSYSTEM
• RECONFIGURABLE FLIGHT CONTROL DESIGN
• INTELLIGENT HYBRID FLIGHT VEHICLE CONTROL SYSTEM DESIGN
• INTERPLANETARY SATELLITE ORBIT DETERMINATION USING GROUND BASED OBSERVATIONS
• Nonlinear analysis & reconfigurable control of AMCA operating at high angles of attack
• Nonlinear analysis and reconfigurable control of AMCA operating at high AOA (Phase - II)

Co-Principal Investigator

• AUTONOMOUS FLIGHT CONTROL DESIGN FOR AURA
• GENERAL MOTORS ECS CRL PROJECTS
• Research on AGV