Vaios Lappas
Cited by
Cited by
Space vehicle design
MD Griffin
AIAA, 2004
Using CubeSat/micro-satellite technology to demonstrate the Autonomous Assembly of a Reconfigurable Space Telescope (AAReST)
C Underwood, S Pellegrino, VJ Lappas, CP Bridges, J Baker
Acta Astronautica 114, 112-122, 2015
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
Direct thrust measurement of a permanent magnet helicon double layer thruster
K Takahashi, T Lafleur, C Charles, P Alexander, RW Boswell, M Perren, ...
Applied Physics Letters 98 (14), 2011
Attitude control for small satellites using control moment gyros
VJ Lappas, WH Steyn, CI Underwood
Acta Astronautica 51 (1-9), 101-111, 2002
Performance characterization of a helicon double layer thruster using direct thrust measurements
S Pottinger, V Lappas, C Charles, R Boswell
Journal of Physics D: Applied Physics 44 (23), 235201, 2011
Spacecraft formation flying using Lorentz forces
MA Peck, B Streetman, CM Saaj, V Lappas
Journal of the British Interplanetary Society 60, 263-267, 2007
Design and development of a gossamer sail system for deorbiting in low earth orbit
JM Fernandez, L Visagie, M Schenk, OR Stohlman, GS Aglietti, ...
Acta Astronautica 103, 204-225, 2014
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
Completely stripped solar sail concept using bi-stable reeled composite booms
JM Fernandez, VJ Lappas, AJ Daton-Lovett
Acta astronautica 69 (1-2), 78-85, 2011
Survey of technology developments in flywheel attitude control and energy storage systems
V Lappas, D Richie, C Hall, J Fausz, B Wilson
Journal of guidance, control, and dynamics 32 (2), 354-365, 2009
Characterising wireless sensor motes for space applications
T Vladimirova, CP Bridges, G Prassinos, X Wu, K Sidibeh, DJ Barnhart, ...
Second NASA/ESA conference on adaptive hardware and systems (AHS 2007), 43-50, 2007
Torque amplification of control moment gyros
VJ Lappas, WH Steyn, CI Underwood
Electronics Letters 38 (15), 1, 2002
A control moment gyro (CMG) based attitude control system (ACS) for agile small satellites
VJ Lappas
PQDT-UK & Ireland, 2002
Drag sails for space debris mitigation
L Visagie, V Lappas, S Erb
Acta Astronautica 109, 65-75, 2015
Solar sails: technology and demonstration status
L Johnson, R Young, N Barnes, L Friedman, V Lappas, C McInnes
International journal of aeronautical and space sciences 13 (4), 421-427, 2012
Redundant reaction wheel torque distribution yielding instantaneous l2 power-optimal spacecraft attitude control
H Schaub, VJ Lappas
Journal of guidance, control, and dynamics 32 (4), 1269-1276, 2009
Spacecraft swarm navigation and control using artificial potential field and sliding mode control
CM Saaj, V Lappas, V Gazi
2006 IEEE International Conference on Industrial Technology, 2646-2651, 2006
A practical small satellite variable-speed control moment gyroscope for combined energy storage and attitude control
DJ Richie, VJ Lappas, G Prassinos
Acta Astronautica 65 (11-12), 1745-1764, 2009
Bistable over the whole length (BOWL) CFRP booms for solar sails
JM Fernandez, A Viquerat, VJ Lappas, AJ Daton-Lovett
Advances in solar sailing, 609-628, 2014
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