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Sensor Fusion Applied to Autonomous Aerial Refueling

Journal of guidance, control, and dynamics, 2009-01, Vol.32 (1), p.262-275

2009

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Fault Detection and Isolation for Deep Space Satellites

Journal of guidance, control, and dynamics, 2009-09, Vol.32 (5), p.1570-1584

2009

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NASA's Lunar Trailblazer Mission: A Pioneering Small Satellite for Lunar Water and Lunar Geology

2022 IEEE Aerospace Conference (AERO), 2022, p.1-14

2022

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Controllable Drogue for Automated Aerial Refueling

Journal of aircraft, 2010-03, Vol.47 (2), p.515-527

2010

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An Instrumentation System Applied to Formation Flight

IEEE transactions on control systems technology, 2007-01, Vol.15 (1), p.75-85

2007

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Optimization and Implementation of Periodic Cruise for a Hypersonic Vehicle

Journal of guidance, control, and dynamics, 2006-09, Vol.29 (5), p.1032-1040

2006

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Hypothesis Testing for Resolving Integer Ambiguity in GPS

Navigation (Washington), 2003, Vol.50 (1), p.45-56

2003

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Minimum and Maximum Endurance Trajectories for Gliding Flight in a Horizontal Plane

Journal of guidance and control, 1979-11, Vol.2 (6), p.457-462

Williamson, Walton E

1979

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Optimal Trajectories for a Ballistic Re-entry Vehicle Recovery System

Journal of guidance and control, 1979-11, Vol.2 (6), p.536-540

Williamson, Walton E

1979

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GNSS Radio Occultation

Position, Navigation, and Timing Technologies in the 21st Century, 2020, p.971-1013

1, 2020

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Maximum-Endurance Return-to-Target Gliding Trajectories

Journal of guidance and control, 1980-09, Vol.3 (5), p.474-477

Williamson, Walton E

1980

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Numerical Derivatives for Parameter Optimization

Journal of guidance and control, 1979-03, Vol.2 (2), p.158-160

1979

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Variable Node Drag Parameterization for Re-entry Trajectory Estimation

Journal of guidance, control, and dynamics, 1982-07, Vol.5 (4), p.321-324

1982

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Instrument Modeling for Aerodynamic Coefficient Identification from Flight Test Data

Journal of guidance and control, 1980-05, Vol.3 (3), p.275-279

1980

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Nonlinear Method for Parameter Identification Applied to a Trajectory Estimation Problem

Journal of guidance, control, and dynamics, 1978-07, Vol.1 (4), p.286-288

1978

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Real time, high accuracy, relative state estimation for multiple vehicle systems

Williamson, Walton Ross

2000

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Re-entry Vehi.cle State and Aerodynamic Coefficient Estimation from Dual Accelerometers

Journal of guidance and control, 1981-09, Vol.4 (5), p.582-583

1981

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A Report on Optimization Techniques at the AIAA Atmospheric Flight Mechanics and Guidance and Control Conference

Optimal control applications & methods, 1982-04, Vol.3 (2), p.203-206

1982

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OPTIMAL THREE DIMENSIONAL REENTRY TRAJECTORIES FOR APOLLO-TYPE VEHICLES

WILLIAMSON, WALTON

1970

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Riccati differential equations

Journal of the Franklin Institute, 1976-10, Vol.302 (4), p.379

Williamson, Walton E.

1976

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A comparison of state space, range space, and carrier phase differential GPS/INS relative navigation

Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334), 2000, Vol.4, p.2932-2938 vol.4

2000

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Carrier phase differential GPS/INS positioning for formation flight

Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251), 1999, Vol.5, p.3665-3670 vol.5

1999

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Riccati differential equations : William T.^Reid. 216 pages, diagrams, 6x9 in. New York, Academic Press Inc. (Mathematics in Science and Industry Series), Vol. 86, 1972. Price, $14.00

Journal of the Franklin Institute, 1976, Vol.302 (4), p.379-379

Williamson, Walton E.

1976

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Developing quality fidelity and engagement measures for complex health interventions

British journal of health psychology, 2020-02, Vol.25 (1), p.39-60

2020

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Mixed-Metal MIL-100(Sc,M) (M=Al, Cr, Fe) for Lewis Acid Catalysis and Tandem CC Bond Formation and Alcohol Oxidation

Chemistry : a European journal, 2014-12, Vol.20 (51), p.17185-17197

2014

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Sensor Fusion Applied to Autonomous Aerial Refueling

Fault Detection and Isolation for Deep Space Satellites

NASA's Lunar Trailblazer Mission: A Pioneering Small Satellite for Lunar Water and Lunar Geology

Controllable Drogue for Automated Aerial Refueling

An Instrumentation System Applied to Formation Flight

Optimization and Implementation of Periodic Cruise for a Hypersonic Vehicle

Hypothesis Testing for Resolving Integer Ambiguity in GPS

Minimum and Maximum Endurance Trajectories for Gliding Flight in a Horizontal Plane

Optimal Trajectories for a Ballistic Re-entry Vehicle Recovery System

GNSS Radio Occultation

Maximum-Endurance Return-to-Target Gliding Trajectories

Numerical Derivatives for Parameter Optimization

Variable Node Drag Parameterization for Re-entry Trajectory Estimation

Instrument Modeling for Aerodynamic Coefficient Identification from Flight Test Data

Nonlinear Method for Parameter Identification Applied to a Trajectory Estimation Problem

Real time, high accuracy, relative state estimation for multiple vehicle systems

Re-entry Vehi.cle State and Aerodynamic Coefficient Estimation from Dual Accelerometers

A Report on Optimization Techniques at the AIAA Atmospheric Flight Mechanics and Guidance and Control Conference

OPTIMAL THREE DIMENSIONAL REENTRY TRAJECTORIES FOR APOLLO-TYPE VEHICLES

Riccati differential equations

A comparison of state space, range space, and carrier phase differential GPS/INS relative navigation

Carrier phase differential GPS/INS positioning for formation flight

Riccati differential equations : William T.^Reid. 216 pages, diagrams, 6x9 in. New York, Academic Press Inc. (Mathematics in Science and Industry Series), Vol. 86, 1972. Price, $14.00

Developing quality fidelity and engagement measures for complex health interventions

Mixed-Metal MIL-100(Sc,M) (M=Al, Cr, Fe) for Lewis Acid Catalysis and Tandem CC Bond Formation and Alcohol Oxidation

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