| 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 | 210 | 2016 |
| 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 | 180 | 2011 |
| 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 | 174 | 2020 |
| Attitude control for small satellites using control moment gyros VJ Lappas, WH Steyn, CI Underwood Acta Astronautica 51 (1-9), 101-111, 2002 | 162 | 2002 |
| 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 | 137 | 2008 |
| 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 | 113 | 2020 |
| 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 | 104 | 1996 |
| 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 | 97 | 2005 |
| A multi-mode attitude determination and control system for small satellites WH Steyn Stellenbosch: Stellenbosch University, 1995 | 94 | 1995 |
| Near-minimum-time eigenaxis rotation maneuvers using reaction wheels WH Steyn Journal of Guidance, Control, and Dynamics 18 (5), 1184-1189, 1995 | 90 | 1995 |
| 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 | 79 | 1999 |
| 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 | 77 | 1994 |
| 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 | 70 | 2017 |
| Torque amplification of control moment gyros VJ Lappas, WH Steyn, CI Underwood Electronics Letters 38 (15), 1, 2002 | 70 | 2002 |
| 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 | 66 | 2020 |
| Practical results on the development of a control moment gyro based attitude control system for agile small satellites VJ Lappas | 53 | 2002 |
| In-orbit attitude performance of the 3-axis stabilised SNAP-1 nanosatellite WH Steyn, Y Hashida | 53 | 2001 |
| An attitude control system for a low-cost Earth observation satellite with orbit maintenance capability W Steyn, Y Hashida | 48 | 1999 |
| An attitude control system and commissioning results of the snap-1 nanosatellite WH Steyn, Y Hashida, V Lappas | 46 | 2000 |
| 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 | 43 | 2011 |
Johan du PreezProfessor of Electrical and Electronic EngineeringVerified email at sun.ac.za
