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Dr. Ali Sarosh

Simulated annealing based artificial bee colony algorithm for global numerical optimization.

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A novel KFCM based fault diagnosis method for unknown faults in satellite reaction wheels

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An improved particle swarm optimizer for parametric optimization of flexible satellite controller

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Counterspace operations and nascent space powers

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A difference-fractional FOM decision method for down-selection of hypersonic compression system conf

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A difference-fractional FOM decision method for down-selection of hypersonic compression system conf

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A configurational aerothermodynamics methodology for derivation of baseline configuration on...

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Case based reasoning support for adaptive FEA: mesh selection for an integrated system

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The GA-ANN expert system for mass-model classification of TSTO surrogates

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Foundations and practical applications of cognitive systems and information processing

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A TIPSO algorithm assessment for aerothermodynamic optimization of hypersonic compression systems

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An improved PSO-SVM approach for multi-faults diagnosis of satellite reaction wheel

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Feasibility assessment of running JP-8 fuel in diesel engine

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A novel KFCM based fault diagnosis method for unknown faults in satellite reaction wheels

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Artificial Bee Colony algorithm for parametric optimization of spacecraft attitude tracking control

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An Aerothermodynamic and Mass-Model Integrated Optimization Framework for Highly-Integrated Forebody

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STS forebody material selection method using integrated aerothermodynamic optimization approach

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Policy Considerations for Nascent Space Powers

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A Cognitive-Heuristic Framework for Optimization of Spaceplane-System Configurations

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Heuristic-intelligent design schemes a solution paradigm for transatmospheric cruiser

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Nascent Space Powers: Some Policy Issues

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Hybrid Assisted Regenerative Turbofan Engine: A case study for XWB-84 Modification

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Space Technology Applications for Maritime Intelligence, Surveillance, and Reconnaissance

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Integration of small telescopes with satellite tracking analytical model for space situational aware

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A Computationally Intelligent Expert System for Design Parameterization of Sub-Orbital Carrier

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A TIPSO-SVM Expert System for Efficient Classification of TSTO Surrogates

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An Aerothermodynamic Design Approach for Scramjet Combustors and Comparative Performance...

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An Aerothermodynamic-CFD Approach for Design of Hydrogen-Fuelled, Constant-Area Scramjet Combustor

For more information on the mentioned research paper, please: 

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Wake reduction in horizontal axis wind turbine: A review of advancements in techniques

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A FOM Based Computational Heat Transfer Method for Aerothermal Analysis of Airborne Electronics LRU

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Wake reduction in horizontal axis wind turbine: A review of advancements in techniques

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Mechanical Components Design for a HARTFE Configuration for Future Aircraft propulsion

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Design of Rocket-Ramjet Integrated System

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Design of Hypersonic Space Transportation System

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Erratum to: A Cognitive-Heuristic Framework for Optimization of Spaceplane-System Configurations

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Modal Analysis of Thin Walled Multi-cell Composite Doubly Tapered Beams of Closed Cross Sections

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An Integrated Design and Intelligent Optimization Framework for Forebody-Inlet Configuration...

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An iterative approach for modal analysis of solid rocket motor incorporating frequency dependent mod

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Structural optimization of elliptical-tip star propellant grain using sub-problem approximation

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Study of Design and Performance Analysis for Comparative Hydrogen-Fuelled Scramjet Propulsion System

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Modal Analysis of Thin Walled Multi-cell Composite Doubly Tapered Beams of Closed Cross Sections

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Robotic Manipulator for Space Debris Mitigation in Low Earth Orbit

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A NOVEL TWO-STEPS PSO ALGORITHM SOLUTION FOR AEROTHERMODYNAMIC OPTIMIZATION PROBLEM

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Parametric Simulations of Dilution of Position (DOP) and Navigation Accuracy Using Satellite Toolkit

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International Journal of Mechanical, Industrial and Aerospace Sciences

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Heuristic-Intelligent Design Schemes

Customers have questions, you have answers. Display the most frequently asked questions, so everybody benefits.

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Conceptual design of independently configurable Mach 6.8 hydrogen fuelled dual mode scramjet

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A Survey of Research Advancement on Unstart Flow Mechanism of The Air-Breathing Hypersonic Inlet

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