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    Browsing by Advisor "Padhi, Radhakant"

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    Now showing items 1-13 of 13

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      • Adaptive and Optimal Control based Artificial Pancreas for Type-1 Diabetes Mellitus Patients 

        Chandrasekhar, Abishek
        This research focuses on the development of adaptive and optimal control algorithms and their implementation to develop Artificial Pancreas (AP) systems for glucose regulation in Type-1 Diabetes Mellitus (T1DM) patients. ...
      • Advanced Guidance and Autopilot Design for Autonomous Lunar Soft-Landing 

        Banerjee, Avijit
        Aiming towards the development of a long-term lunar research base for scientific exploration of futuristic objectives, soft-landing on the Moon has gained renewed interest worldwide. This work focuses on optimal guidance ...
      • Advanced Optimal Control Design for Nonlinear Systems including Impulsive Inputs with Applications to Automatic Cancer Treatment 

        Sakode, Chandrashekar M (2018-08-14)
        The motivation of this research is to propose innovative nonlinear and optimal control design algorithms, which can be used in real life. The algorithms need to be computationally efficient, should deal with control ...
      • Advanced Optimal Spacecraft Guidance For Terminal Phase Rendezvous and Docking 

        Lagisetty, Ravikumar
        There have been growing interest in Rendezvous and Docking (RVD) missions for on-orbit refueling, on-orbit servicing, orbital debris removal, etc. A very important requirement in RVD missions is soft-docking at the terminal ...
      • Autonomous Landing Of Unmanned Aerial Vehicles 

        Singh, Shashiprakash (2010-03-26)
        In this thesis the problem of autonomous landing of an unmanned aerial vehicle named AE-2 is addressed. The guidance and control technique is developed and demonstrated through numerical simulation results. The complete ...
      • Constrained Adaptive Control of Nonlinear Systems with Application to Hypersonic Vehicles 

        Sachan, Kapil
        Constraints in input, output, and states are evident in most of the practical systems. Explicitly incorporating these constraints into the control design process leads to its superior performance in general. Therefore, ...
      • Constrained Optimal Guidance Design of Interceptors for High-Speed Ballistic Targets 

        Mondal, Sabyasachi
        In this thesis, optimal control theory has been applied to design constrained terminal guidance algorithms for interceptor to destroy incoming high speed ballistic targets. There exist several optimal guidance algorithms ...
      • A Control Systems Approach to Understanding Saccadic Eye Movements 

        Varsha, V
        The oculomotor system is extensively studied using concepts of control theory like optimal control, feedback control, and predictive control. But these studies have largely been restricted to investigating the central ...
      • Innovative Optimal Guidance of Spacecrafts for Soft-Landing on Atmosphere-less Celestial Bodies 

        Mathavaraj, S
        Nonlinear trajectory optimization based optimal guidance schemes are presented in this thesis for soft-landing of spacecrafts on atmosphere-less celestial bodies. First, a pseudo-spectral philosophy based multi-phase ...
      • Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines 

        Maity, Arnab (2016-07-11)
        A new suboptimal guidance law design approach for aerospace vehicles is proposed in this thesis, followed by an advanced control design for supersonic air-breathing engines. The guidance law is designed using the newly ...
      • Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance 

        Chawla, Charu (2012-04-24)
        UAVs employed for low altitude jobs are more liable to collide with the urban structures on their way to the goal point. In this thesis, the problem of reactive obstacle avoidance is addressed by an innovative partial ...
      • Robust Station-keeping and High-Precision Attitude Control for a Spacecraft on Sun–Earth L1 Halo Orbit 

        Vutukuri, Srianish
        The halo orbits around the Sun-Earth L1 Lagrange point form an ideal location for deploying a solar observation spacecraft as they offer uninterrupted, long-duration visibility of the Sun. However, the complex orbital and ...
      • Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors 

        Das, Priya G (2011-03-17)
        To address the concern of classical guidance and control designs (where guidance and control loops are designed separately in an “outer loop – inner loop” structure), integrated guidance and control (IGC) ideas have been ...

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