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What Is Control?

Journal of guidance, control, and dynamics, 2023-10, Vol.46 (10), p.1857-1859

Kluever, Craig A.

2023

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Entry Guidance Performance for Mars Precision Landing

Journal of guidance, control, and dynamics, 2008-11, Vol.31 (6), p.1537-1544

Kluever, C. A.

2008

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Low-Thrust Guidance for Geocentric Transfers Using Single-Rotation-Axis Steering

Journal of guidance, control, and dynamics, 2022-10, Vol.45 (10), p.1927-1933

Kluever, Craig A.

2022

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Simple Analytical Terminal Area Guidance for an Unpowered Reusable Launch Vehicle

Journal of guidance, control, and dynamics, 2022-04, Vol.45 (4), p.740-747

Kluever, Craig A.

2022

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Low-Thrust Geostationary Transfer Orbit (LT2GEO) Radiation Environment and Associated Solar Array Degradation Modeling and Ground Testing

IEEE transactions on nuclear science, 2014-12, Vol.61 (6), p.3348-3355

2014

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Terminal Guidance for an Unpowered Reusable Launch Vehicle with Bank Constraints

Journal of guidance, control, and dynamics, 2007-01, Vol.30 (1), p.162-168

Kluever, C. A

2007

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Entry Guidance Using Analytical Atmospheric Skip Trajectories

Journal of guidance, control, and dynamics, 2008-09, Vol.31 (5), p.1531-1535

Kluever, C. A.

2008

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Designing Transfers to Geostationary Orbit Using Combined Chemical–Electric Propulsion

Journal of spacecraft and rockets, 2015-07, Vol.52 (4), p.1144-1151

Kluever, Craig A.

2015

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Unpowered Approach and Landing Guidance Using Trajectory Planning

Journal of guidance, control, and dynamics, 2004-11, Vol.27 (6), p.967-974

Kluever, C. A

2004

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Analytical Earth-Aerocapture Guidance with Near-Optimal Performance

Journal of guidance, control, and dynamics, 2021-01, Vol.44 (1), p.45-56

2021

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HESI workshop summary: Interpretation of developmental and reproductive toxicity endpoints and the impact on data interpretation of adverse events

Birth defects research, 2024-02, Vol.116 (2), p.e2311-n/a

2024

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Using Edelbaum's Method to Compute Low-Thrust Transfers with Earth-Shadow Eclipses

Journal of guidance, control, and dynamics, 2011-01, Vol.34 (1), p.300-303

Kluever, Craig A.

2011

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Unpowered Approach and Landing Guidance with Normal Acceleration Limitations

Journal of guidance, control, and dynamics, 2007-05, Vol.30 (3), p.882-885

Kluever, C. A

2007

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Efficient Computation of Optimal Interplanetary Trajectories Using Solar Electric Propulsion

Journal of guidance, control, and dynamics, 2015-05, Vol.38 (5), p.821-830

Kluever, Craig A.

2015

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Optimal Geostationary Orbit Transfers Using Onboard Chemical-Electric Propulsion

Journal of spacecraft and rockets, 2012-11, Vol.49 (6), p.1174-1182

Kluever, Craig A.

2012

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Analytic Orbital Averaging Technique for Computing Tangential-Thrust Trajectories

Journal of guidance, control, and dynamics, 2005-11, Vol.28 (6), p.1320-1323

2005

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Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle

Journal of guidance, control, and dynamics, 2015-11, Vol.38 (11), p.2057-2066

2015

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Rapid Evaluation of Low-Thrust Transfers from Elliptical Orbits to Geostationary Orbit

Journal of spacecraft and rockets, 2020-09, Vol.57 (5), p.898-906

2020

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Interplanetary Mission Design Using Differential Evolution

Journal of spacecraft and rockets, 2007-09, Vol.44 (5), p.1060-1070

2007

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Analytical Guidance for Mars Aerocapture via Drag Modulation

The Journal of the astronautical sciences, 2022-06, Vol.69 (3), p.857-878

2022

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Approach and Landing Guidance for an Unpowered Gliding Vehicle

Journal of guidance, control, and dynamics, 2020-12, Vol.43 (12), p.2366-2371

2020

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Correction to: Analytical Guidance for Mars Aerocapture via Drag Modulation

The Journal of the astronautical sciences, 2022, Vol.69 (3), p.954-954

2022

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Solar-Cell Degradation Model for Trajectory Optimization Methods

Journal of spacecraft and rockets, 2019-05, Vol.56 (3), p.844-853

2019

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Simple Guidance Scheme for Low-Thrust Orbit Transfers

Journal of guidance, control, and dynamics, 1998-11, Vol.21 (6), p.1015-1017

Kluever, Craig A

1998

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Direct Approach for Computing Near-Optimal Low-Thrust Earth-Orbit Transfers

Journal of spacecraft and rockets, 1998-07, Vol.35 (4), p.509-515

1998

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What Is Control?

Entry Guidance Performance for Mars Precision Landing

Low-Thrust Guidance for Geocentric Transfers Using Single-Rotation-Axis Steering

Simple Analytical Terminal Area Guidance for an Unpowered Reusable Launch Vehicle

Low-Thrust Geostationary Transfer Orbit (LT2GEO) Radiation Environment and Associated Solar Array Degradation Modeling and Ground Testing

Terminal Guidance for an Unpowered Reusable Launch Vehicle with Bank Constraints

Entry Guidance Using Analytical Atmospheric Skip Trajectories

Designing Transfers to Geostationary Orbit Using Combined Chemical–Electric Propulsion

Unpowered Approach and Landing Guidance Using Trajectory Planning

Analytical Earth-Aerocapture Guidance with Near-Optimal Performance

HESI workshop summary: Interpretation of developmental and reproductive toxicity endpoints and the impact on data interpretation of adverse events

Using Edelbaum's Method to Compute Low-Thrust Transfers with Earth-Shadow Eclipses

Unpowered Approach and Landing Guidance with Normal Acceleration Limitations

Efficient Computation of Optimal Interplanetary Trajectories Using Solar Electric Propulsion

Optimal Geostationary Orbit Transfers Using Onboard Chemical-Electric Propulsion

Analytic Orbital Averaging Technique for Computing Tangential-Thrust Trajectories

Approach and Landing Range Guidance for an Unpowered Reusable Launch Vehicle

Rapid Evaluation of Low-Thrust Transfers from Elliptical Orbits to Geostationary Orbit

Interplanetary Mission Design Using Differential Evolution

Analytical Guidance for Mars Aerocapture via Drag Modulation

Approach and Landing Guidance for an Unpowered Gliding Vehicle

Correction to: Analytical Guidance for Mars Aerocapture via Drag Modulation

Solar-Cell Degradation Model for Trajectory Optimization Methods

Simple Guidance Scheme for Low-Thrust Orbit Transfers

Direct Approach for Computing Near-Optimal Low-Thrust Earth-Orbit Transfers

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