Dr. Frederick A. Leve
Dr. Frederick A. Leve
Air Force Office of Scientific Research
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Cited by
Cited by
On the use of simulation in robotics: Opportunities, challenges, and suggestions for moving forward
HS Choi, C Crump, C Duriez, A Elmquist, G Hager, D Han, F Hearl, ...
Proceedings of the National Academy of Sciences 118 (1), e1907856118, 2021
Spacecraft momentum control systems
FA Leve, BJ Hamilton, MA Peck
Springer, 2015
Hybrid steering logic for single-gimbal control moment gyroscopes
FA Leve, NG Fitz-Coy
Journal of guidance, control, and dynamics 33 (4), 1202-1212, 2010
Astrometric and photometric data fusion for inactive space object mass and area estimation
R Linares, MK Jah, JL Crassidis, FA Leve, T Kelecy
Acta Astronautica 99, 1-15, 2014
Adaptive neural network-based satellite attitude control in the presence of CMG uncertainty
W MacKunis, F Leve, PM Patre, N Fitz-Coy, WE Dixon
Aerospace Science and Technology 54, 218-228, 2016
Constrained spacecraft relative motion planning exploiting periodic natural motion trajectories and invariance
GR Frey, CD Petersen, FA Leve, IV Kolmanovsky, AR Girard
Journal of Guidance, Control, and Dynamics 40 (12), 3100-3115, 2017
Evaluation of steering algorithm optimality for single-gimbal control moment gyroscopes
FA Leve
IEEE Transactions on Control Systems Technology 22 (3), 1130-1134, 2013
Model predictive control of an underactuated spacecraft with two reaction wheels
CD Petersen, F Leve, I Kolmanovsky
Journal of Guidance, Control, and Dynamics 40 (2), 320-332, 2017
Spacecraft constrained attitude control using positively invariant constraint admissible sets on SO(3) × ℝ3
A Weiss, F Leve, M Baldwin, JR Forbes, I Kolmanovsky
2014 American Control Conference, 4955-4960, 2014
Spacecraft relative attitude formation tracking on SO (3) based on line-of-sight measurements
TH Wu, B Flewelling, F Leve, T Lee
2013 American Control Conference, 4820-4825, 2013
Space object mass-specific inertia matrix estimation from photometric data
R Linares, FA Leve, MK Jan, JL Crassidis
Advances in the Astronautical Sciences 144, 41-54, 2012
Attitude control system for small satellites
V Nagabhushan, NG Fitz-Coy, FA Leve
US Patent 9,199,746, 2015
A slowly rotating hollow sphere in a magnetic field: First steps to de-spin a space object
RC Youngquist, MA Nurge, SO Starr, FA Leve, M Peck
American Journal of Physics 84 (3), 181-191, 2016
Lagrangian mechanics and Lie group variational integrators for spacecraft with imbalanced reaction wheels
T Lee, F Leve
2014 American Control Conference, 3122-3127, 2014
Minimum error dissipative power reduction control allocation via lexicographic convex optimization for momentum control systems
D Dueri, F Leve, B Açıkmeşe
IEEE Transactions on Control Systems Technology 24 (2), 678-686, 2015
A thick-walled sphere rotating in a uniform magnetic field: The next step to de-spin a space object
MA Nurge, RC Youngquist, RA Caracciolo, M Peck, FA Leve
American Journal of Physics 85 (8), 596-610, 2017
Dynamics and control of spacecraft with a generalized model of variable speed control moment gyroscopes
SP Viswanathan, AK Sanyal, F Leve, NH McClamroch
Journal of Dynamic Systems, Measurement, and Control 137 (7), 071003, 2015
Development of the spacecraft orientation buoyancy experimental kiosk
FA Leve
Department of Mechanical and Aerospace Engineering, University of Florida …, 2008
Recovering linear controllability of an underactuated spacecraft by exploiting solar radiation pressure
CD Petersen, F Leve, M Flynn, I Kolmanovsky
Journal of Guidance, Control, and Dynamics 39 (4), 826-837, 2016
A Scalable Control Moment Gyro Design for Attitude Control of Micro-, Nano-, and Pico-Class Satellites (AAS 07-041)
F Leve, A Tatsch, N Fitz-Coy
Advances in the Astronautical Sciences 128, 235, 2007
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