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Willem Herman Steyn
Willem Herman Steyn
Professor in Electrical and Electronic Engineering, University of Stellenbosch
Verified email at sun.ac.za
Title
Cited by
Cited by
Year
RemoveDEBRIS: An in-orbit active debris removal demonstration mission
JL Forshaw, GS Aglietti, N Navarathinam, H Kadhem, T Salmon, ...
Acta Astronautica 127, 448-463, 2016
1882016
CubeSail: A low cost CubeSat based solar sail demonstration mission
V Lappas, N Adeli, L Visagie, J Fernandez, T Theodorou, W Steyn, ...
Advances in Space Research 48 (11), 1890-1901, 2011
1722011
Attitude control for small satellites using control moment gyros
VJ Lappas, WH Steyn, CI Underwood
Acta Astronautica 51 (1-9), 101-111, 2002
1632002
The active space debris removal mission RemoveDebris. Part 2: In orbit operations
GS Aglietti, B Taylor, S Fellowes, T Salmon, I Retat, A Hall, T Chabot, ...
Acta Astronautica 168, 310-322, 2020
1472020
Kalman filter configurations for a low-cost loosely integrated inertial navigation system on an airship
J Bijker, W Steyn
Control Engineering Practice 16 (12), 1509-1518, 2008
1322008
A new unified approach to power quality management
A van Zyl, JHR Enslin, R Spée
IEEE Transactions on Power Electronics 11 (5), 691-697, 1996
1031996
Design and testing of a control moment gyroscope cluster for small satellites
V Lappas, WH Steyn, C Underwood
Journal of Spacecraft and Rockets 42 (4), 729-739, 2005
1002005
The active space debris removal mission RemoveDebris. Part 1: From concept to launch
JL Forshaw, GS Aglietti, S Fellowes, T Salmon, I Retat, A Hall, T Chabot, ...
Acta Astronautica 168, 293-309, 2020
952020
A multi-mode attitude determination and control system for small satellites
WH Steyn
Stellenbosch: Stellenbosch University, 1995
951995
Near-minimum-time eigenaxis rotation maneuvers using reaction wheels
WH Steyn
Journal of Guidance, Control, and Dynamics 18 (5), 1184-1189, 1995
901995
Optimal combined reaction-wheel momentum management for earth-pointing satellites
X Chen, WH Steyn, S Hodgart, Y Hashida
Journal of guidance, control, and dynamics 22 (4), 543-550, 1999
761999
Comparison of low-earth-orbit satellite attitude controllers submitted to controllability constraints
WH Steyn
Journal of Guidance, Control, and Dynamics 17 (4), 795-804, 1994
751994
Torque amplification of control moment gyros
VJ Lappas, WH Steyn, CI Underwood
Electronics Letters 38 (15), 1, 2002
702002
Final payload test results for the RemoveDebris active debris removal mission
JL Forshaw, GS Aglietti, T Salmon, I Retat, M Roe, C Burgess, T Chabot, ...
Acta Astronautica 138, 326-342, 2017
662017
RemoveDEBRIS: An in-orbit demonstration of technologies for the removal of space debris
GS Aglietti, B Taylor, S Fellowes, S Ainley, D Tye, C Cox, A Zarkesh, ...
The Aeronautical Journal 124 (1271), 1-23, 2020
542020
Practical results on the development of a control moment gyro based attitude control system for agile small satellites
VJ Lappas
522002
In-orbit attitude performance of the 3-axis stabilised SNAP-1 nanosatellite
WH Steyn, Y Hashida
502001
An attitude control system for a low-cost Earth observation satellite with orbit maintenance capability
W Steyn, Y Hashida
461999
An attitude control system and commissioning results of the snap-1 nanosatellite
WH Steyn, Y Hashida, V Lappas
452000
Cubesat solar sail 3-axis stabilization using panel translation and magnetic torquing
WH Steyn, V Lappas
Aerospace Science and Technology 15 (6), 476-485, 2011
412011
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