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    Artificial Neural Network Approach For Characterization Of Acoustic Emission Sources From Complex Noisy Data 

    Bhat, Chandrashekhar (Indian Institute of Science, 2006-12-14)
    Safety and reliability are prime concerns in aircraft performance due to the involved costs and risk to lives. Despite the best efforts in design methodology, quality evaluation in production and structural integrity ...

    Computational Studies On Certain Problems Of Combustion Instability In Solid Propellants 

    Anil Kumar, K R (Indian Institute of Science, 2006-11-17)
    This thesis presents the results and analyses of computational studies on certain problems of combustion instability in solid propellants. Specifically, effects of relaxing certain assumptions made in previous models of ...

    An Autonomous Guidance Scheme For Orbital Rendezvous 

    Shankar, G S (Indian Institute of Science, 2005-07-15)
    The word 'rendezvous' implies a pre-arranged meeting between two entities for a specific purpose. This term is used in the study of spacecraft operations, to describe a set of maneuvers performed by two spacecraft in order ...

    NEW PERSPECTIVES FOR ANALYZING THE BREAKUP, ENVIRONMENT, EVOLUTION, COLLISION RISK AND REENTRY OF SPACE DEBRIS OBJECTS 

    Anilkumar, A K (Indian Institute of Science, 2005-03-10)
    In the space surrounding the earth there are two major regions where orbital debris causes concern. They are the Low Earth Orbits (LEO) up to about 2000 km, and Geosynchronous Orbits (GEO) at an altitude of around 36000 ...

    Ultra High Compression For Weather Radar Reflectivity Data 

    Makkapati, Vishnu Vardhan (2007-10-09)
    Weather is a major contributing factor in aviation accidents, incidents and delays. Doppler weather radar has emerged as a potent tool to observe weather. Aircraft carry onboard radars but their range and angular resolution ...

    Application Of Controlled Random Search Optimization Technique In MMLE With Process Noise 

    Anilkumar, A K (Indian Institute of Science, 2006-08-08)
    Generally in most of the applications of estimation theory using the Method of Maximum Likelihood Estimation (MMLE) to dynamical systems one deals with a situation where only the measurement noise alone is present. However ...

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    AuthorAnilkumar, A K (2)Anil Kumar, K R (1)Bhat, Chandrashekhar (1)Makkapati, Vishnu Vardhan (1)Shankar, G S (1)Subject
    Aerospace Engineering (6)
    Kalman Filter (2)Acoustic Emission (1)AE Signal Characterization (1)Aircraft - Random Search Optimization (1)Aircraft Noise (1)Artificial Neural Networks (ANN) (1)ASSEMBLE Model (1)Autonomous Control (1)Aviation Meteorology (1)... View MoreDate Issued2006 (3)2005 (2)2007 (1)Has File(s)Yes (6)

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