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Impact-time-control guidance law for anti-ship missiles

IEEE transactions on control systems technology, 2006-03, Vol.14 (2), p.260-266

2006

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Revisiting the Resazurin-Based Sensing of Cellular Viability: Widening the Application Horizon

Biosensors (Basel), 2022-03, Vol.12 (4), p.196

2022

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Guidance law switching logic considering the seeker's field-of-view limits

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2009-08, Vol.223 (8), p.1049-1058

2009

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Moderation of Classic Social Psychological Effects by Demographics in the U.S. Adult Population: New Opportunities for Theoretical Advancement

Journal of personality and social psychology, 2019-12, Vol.117 (6), p.e84-e99

2019

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Satellite formation flying using along-track thrust

Acta astronautica, 2007-10, Vol.61 (7), p.553-564

2007

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Missile acceleration controller design using proportional–integral and non-linear dynamic control design method

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2012-08, Vol.226 (8), p.882-897

2012

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A Continuous-Time, Latent-Variable Model of Time Series Data

Political analysis, 2015-04, Vol.23 (2), p.278-298

Tahk, Alexander M.

2015

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Satellite attitude stabilization using solar radiation pressure and magnetotorquer

Control engineering practice, 2009-02, Vol.17 (2), p.267-279

2009

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Optimal Stabilization of Takagi-Sugeno Fuzzy Systems with Application to Spacecraft Control

Journal of guidance, control, and dynamics, 2001-07, Vol.24 (4), p.767-777

2001

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Recursive time-to-go estimation for homing guidance missiles

IEEE transactions on aerospace and electronic systems, 2002-01, Vol.38 (1), p.13-24

2002

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Ionic electroactive polymer control using co-evolutionary optimisation

Electronics letters, 2007-08, Vol.43 (16), p.859-860

2007

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Design and analysis of optimal controller for fuzzy systems with input constraint

IEEE transactions on fuzzy systems, 2004-12, Vol.12 (6), p.766-779

2004

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Multi-model approaches to three-axis missile autopilot design under aerodynamic roll angle uncertainty

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2012-09, Vol.226 (9), p.1061-1077

2012

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Coevolutionary augmented Lagrangian methods for constrained optimization

IEEE transactions on evolutionary computation, 2000-07, Vol.4 (2), p.114-124

2000

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Aerodynamic coupling model development and autopilot design for highly manoeuvring skid-to-turn missiles

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2012-05, Vol.226 (5), p.498-509

2012

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Target tracking problems subject to kinematic constraints

IEEE transactions on automatic control, 1990-03, Vol.35 (3), p.324-326

1990

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Adaptive sliding mode control robust to actuator faults

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2007-02, Vol.221 (1), p.129-144

2007

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New attitude control approach for satellites in elliptic orbits using solar radiation pressure

Acta astronautica, 2006-09, Vol.59 (6), p.462-473

2006

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Optimal Guidance Laws with Terminal Impact Angle Constraint

Journal of guidance, control, and dynamics, 2005-07, Vol.28 (4), p.724-732

2005

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Three-dimensional midcourse guidance using neural networks for interception of ballistic targets

IEEE transactions on aerospace and electronic systems, 2002-04, Vol.38 (2), p.404-414

2002

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Acceleration of the convergence speed of evolutionary algorithms using multi-layer neural networks

Engineering optimization, 2003-02, Vol.35 (1), p.91-102

2003

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Institutions and Equilibrium in the United States Supreme Court

The American political science review, 2007-11, Vol.101 (4), p.811-825

2007

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What Can We Learn About the Ideology of the Newest Supreme Court Justices?

PS, political science & politics, 2011-07, Vol.44 (3), p.524-529

2011

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Practical dual-control guidance using adaptive intermitent maneuver strategy

Journal of guidance, control, and dynamics, 2001-01, Vol.24 (5), p.1009-1015

2001

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Nonlinear Momentum Transfer Control of Spacecraft by Feedback Linearization

Journal of spacecraft and rockets, 2002-11, Vol.39 (6), p.866-873

2002

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Impact-time-control guidance law for anti-ship missiles

Revisiting the Resazurin-Based Sensing of Cellular Viability: Widening the Application Horizon

Guidance law switching logic considering the seeker's field-of-view limits

Moderation of Classic Social Psychological Effects by Demographics in the U.S. Adult Population: New Opportunities for Theoretical Advancement

Satellite formation flying using along-track thrust

Missile acceleration controller design using proportional–integral and non-linear dynamic control design method

A Continuous-Time, Latent-Variable Model of Time Series Data

Satellite attitude stabilization using solar radiation pressure and magnetotorquer

Optimal Stabilization of Takagi-Sugeno Fuzzy Systems with Application to Spacecraft Control

Recursive time-to-go estimation for homing guidance missiles

Ionic electroactive polymer control using co-evolutionary optimisation

Design and analysis of optimal controller for fuzzy systems with input constraint

Multi-model approaches to three-axis missile autopilot design under aerodynamic roll angle uncertainty

Coevolutionary augmented Lagrangian methods for constrained optimization

Aerodynamic coupling model development and autopilot design for highly manoeuvring skid-to-turn missiles

Target tracking problems subject to kinematic constraints

Adaptive sliding mode control robust to actuator faults

New attitude control approach for satellites in elliptic orbits using solar radiation pressure

Optimal Guidance Laws with Terminal Impact Angle Constraint

Three-dimensional midcourse guidance using neural networks for interception of ballistic targets

Acceleration of the convergence speed of evolutionary algorithms using multi-layer neural networks

Institutions and Equilibrium in the United States Supreme Court

What Can We Learn About the Ideology of the Newest Supreme Court Justices?

Practical dual-control guidance using adaptive intermitent maneuver strategy

Nonlinear Momentum Transfer Control of Spacecraft by Feedback Linearization

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