Faculty

Institution

Unit

Venue

Bruce A Conway

Professor Emeritus

UIUC

Affiliations

The Grainger College of Engineering

Aerospace Engineering

Department of Aerospace Engineering

Bruce A Conway is currently serving as an Aerospace Engineering Professor Emeritus at Uiuc.

Honors

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Experiences

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Education

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Bruce A Conway

UIUC

Professor Emeritus

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aerospace engineering trajectory optimization applied mathematics aerospace systems engineering control optimization trajectory planning control systems computational optimization design optimization navigation engineering optimization space exploration automatic control numerical analysis global optimization guidance system mathematical optimization propulsion evolutionary computation swarm intelligence orbit determination dynamical systems numerical mathematics space mission design spacecraft attitude control vehicle system dynamics genetic algorithms celestial mechanics planetary sciences numerical algorithms aircraft path planning numerical computation system optimization earth-moon system evolutionary programming optimal control robust nonlinear control multidisciplinary optimization space engineering formation flying swarm dynamic particle swarm optimization optimal trajectories dynamic optimization differential games impulsive system pde-constrained optimization aerospace systems firefly algorithm control system technology boundary value problems astronautics differential evolution space technology aerospace technology uncertainty management engineering judgement uncertainty modeling continuous optimization hybrid optimization technique hypervelocity impacts hybrid optimal control optimal interception direct optimization quadrature rule periodic orbits space trajectories spacecraft trajectory optimization numerical method direct method mission designer optimal trajectory bounded-impulse trajectory models continuous thrust

Notable Scholarly Works

Notable Federal Grants

Collaborators

Optimal Combined Impulsive/Low-Thrust Trajectories for Asteroid Deflection via Kinetic Impact. Acta Astronautica (2024)

Bruce A. ConwayAlessia SpezialeLudovica Malagni

hypervelocity impactsguidance systemasteroidspropulsiontrajectory optimizationaerospace engineeringaerospacekinetic impactapplied mathematics

Globally Optimal Nonlinear Control via Kriging of Hjb Viscosity Solutions on Quasi-Monte Carlo Grids. J. of Guidance, Control & Dynamics (2019)

Bruce A Conway

quasi-monte carlo gridsnonlinear controlmathematical optimizationoptimal nonlinear controlnonlinear systemscontrol optimizationpde-constrained optimizationhjb viscosity solutionsnonlinear analysisapplied mathematicsnonlinear dynamicsengineeringstochastic partial differential equations

Optimal Nonlinear Control Using Hamilton–Jacobi–Bellman Viscosity Solutions on Unstructured Grids. Journal of Guidance Control and Dynamics (2019)

Christian M. ChilanBruce A. Conway

systems engineeringcontrol systemsnonlinear controloptimal controlcomplex systemspde viscosity solutionsnonlinear systemscontrol optimizationpde-constrained optimizationnonlinear analysisautomatic controlrobust nonlinear controldifferential equationsnonlinear dynamicsapplied mathematicsnonlinear optimization

Analytic Gradient Computation for Bounded-Impulse Trajectory Models Using Two-Sided Shooting. Journal of Guidance Control and Dynamics (2018)

Donald H. EllisonBruce A. ConwayJacob A. EnglanderMartin T. Ozimek

control systemsnumerical analysisderivative-free optimizationtrajectory optimizationmultibody system dynamicanalytic gradient computationrobust nonlinear controlaerospace engineeringaerospacecomplex partial derivativesbounded-impulse trajectory modelsapplied mathematics

Application and Analysis of Bounded-Impulse Trajectory Models With Analytic Gradients. Journal of Guidance Control and Dynamics (2018)

Donald H. EllisonBruce A. ConwayJacob A. EnglanderMartin T. Ozimek

systems engineeringcontrol systemsengineering optimizationnumerical mathematicsnumerical analysisanalytic gradientsanalytic jacobiancontrol optimizationpde-constrained optimizationmodeling and simulationtrajectory optimizationaerospace engineeringaerospacebounded-impulse trajectory modelsapplied mathematics

A Time-Regularized, Multiple Gravity-Assist Low-Thrust, Bounded-Impulse Model for Trajectory Optimization. (2017)

Donald H. EllisonJacob A. EnglanderBruce A. Conway

temporal spacingsystems engineeringcontrol systemsorbit determinationguidance systemcontrol optimizationdynamical systemstrajectory optimizationautomatic controltrajectory planningaerospace engineeringgeneralized anomalyaerospacekepler propagator

Optimal Trajectories for Hyperbolic Rendezvous With Earth–Mars Cycling Spacecraft. Journal of Guidance Control and Dynamics (2017)

Mauro PontaniBruce A. Conway

astronauticstaxi vehicle trajectoriesswarm intelligenceparticle swarmspace mission designspace explorationpropulsionglobal optimizationtrajectory optimizationoptimal trajectoriestrajectory planningaerospace engineeringapplied mathematics

Automated Solution of the Low-Thrust Interplanetary Trajectory Problem. Journal of Guidance Control and Dynamics (2016)

Jacob A. EnglanderBruce A. Conway

systems engineeringcontrol systemsdesign optimizationcomputational optimizationautomated solutionnavigationspace mission designspace explorationguidance systemcontrol system technologycontrol optimizationtrajectory optimizationautomatic controltrajectory planningaerospace engineeringmission designermission design problemaerospace

Evolutionary and Heuristic Methods Applied to Problems in Optimal Control. Springer optimization and its applications (2016)

Bruce A. Conway

system optimizationdesign optimizationmathematical optimizationevolutionary programmingoptimal controlcontrol optimizationevolutionary computationhybrid optimization techniqueintelligent optimizationapplied mathematicsevolutionary intelligenceevolution-based methodoperations research

Numerical Computation of a Continuous-Thrust State Transition Matrix Incorporating Accurate Hardware and Ephemeris Models. AAS/AIAA Space Flight Mechanics Meeting (2015)

Donald EllisonBruce ConwayJacob Englander

numerical mathematicsnumerical analysisnumerical algorithmspower hardward modelflight derivativestrajectory optimizationaerospace engineeringnumerical computationaerospacestate transition matrixapplied mathematics

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Bruce A Conway

Professor Emeritus

UIUC

Affiliations

The Grainger College of Engineering

Aerospace Engineering

Department of Aerospace Engineering

Bruce A Conway is currently serving as an Aerospace Engineering Professor Emeritus at Uiuc.

Honors

Create free account to unlock more features

Experiences

Create free account to unlock more features

Education

Create free account to unlock more features

Bruce A Conway

UIUC

Professor Emeritus

You can click a keyword to filter the displayed items

Notable Scholarly Works

Notable Federal Grants

Collaborators

Optimal Combined Impulsive/Low-Thrust Trajectories for Asteroid Deflection via Kinetic Impact. Acta Astronautica (2024)

Bruce A. ConwayAlessia SpezialeLudovica Malagni

hypervelocity impactsguidance systemasteroidspropulsiontrajectory optimizationaerospace engineeringaerospacekinetic impactapplied mathematics

Globally Optimal Nonlinear Control via Kriging of Hjb Viscosity Solutions on Quasi-Monte Carlo Grids. J. of Guidance, Control & Dynamics (2019)

Bruce A Conway

Optimal Nonlinear Control Using Hamilton–Jacobi–Bellman Viscosity Solutions on Unstructured Grids. Journal of Guidance Control and Dynamics (2019)

Christian M. ChilanBruce A. Conway

Analytic Gradient Computation for Bounded-Impulse Trajectory Models Using Two-Sided Shooting. Journal of Guidance Control and Dynamics (2018)

Donald H. EllisonBruce A. ConwayJacob A. EnglanderMartin T. Ozimek

Application and Analysis of Bounded-Impulse Trajectory Models With Analytic Gradients. Journal of Guidance Control and Dynamics (2018)

Donald H. EllisonBruce A. ConwayJacob A. EnglanderMartin T. Ozimek

A Time-Regularized, Multiple Gravity-Assist Low-Thrust, Bounded-Impulse Model for Trajectory Optimization. (2017)

Donald H. EllisonJacob A. EnglanderBruce A. Conway

Optimal Trajectories for Hyperbolic Rendezvous With Earth–Mars Cycling Spacecraft. Journal of Guidance Control and Dynamics (2017)

Mauro PontaniBruce A. Conway

Automated Solution of the Low-Thrust Interplanetary Trajectory Problem. Journal of Guidance Control and Dynamics (2016)

Jacob A. EnglanderBruce A. Conway

Evolutionary and Heuristic Methods Applied to Problems in Optimal Control. Springer optimization and its applications (2016)

Bruce A. Conway

Numerical Computation of a Continuous-Thrust State Transition Matrix Incorporating Accurate Hardware and Ephemeris Models. AAS/AIAA Space Flight Mechanics Meeting (2015)

Donald EllisonBruce ConwayJacob Englander

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