Professor Vaios Lappas
Email: v.lappas@surrey.ac.uk
Phone: Work: 01483 68 3412
Room no: BA U
Further information
Biography
Vaios graduated with a Bachelor in Aerospace Engineering from Ryerson University, Toronto, Canada in 1998. His thesis involved designing a Single Stage to Orbit Simulator merging animation and modelling techniques. He went on to do a Masters of Space Studies at the International Space University, Strasbourg, France and graduated in 1999. His master’s thesis took place at the Systems Engineering Division of NASA’s Goddard Space Flight Center (GSFC) and Vaios worked on flight dynamics analyses for the Space technology ST-5 nanosatellite program. Vaios went on to do his PhD in 1999 at the Surrey Space Centre, School of Electronics and Physical Sciences, University of Surrey. He completed his PhD in October 2002 on ‘A Control Moment Gyroscope (CMG) based Attitude Control Subsystem (ACS) for Agile Small Satellites’. During his PhD Vaios also worked on the attitude control of the SNAP-1 nanosatellite program and was a teaching assistant for various courses. From 2002 till the end of 2004 Vaios was a research fellow at the Surrey Space Centre, working on various topics including CMGs, solar sail systems design, solar sail attitude control and Mars ascent vehicles, research that was funded by the European Space Agency. Since December 1, 2004 Vaios was appointed lecturer in Attitude/Orbit Control Systems.
Research Interests
Research in Space systems at Surrey is dominated by practical results. Having contributed to the design and launch of 26 spacecraft (2006) SSC has a strong practical perspective in space research. Vaios’s research is mainly focused on 3 areas: (i) attitude control and determination (ii) advanced concepts and (iii) propulsion.
Control Moment Gyroscopes (CMGs)
Vaios has developed these small yet powerful actuators for the next generation of agile spacecraft. CMGs are usually complex and expensive and have flown on space stations and military spacecraft. Developments in microelectronics and mechatronics has enabled a new approach towards the design of smaller, affordable and low cost CMGs. Vaios demonstrated the viability of CMGs for small satellites and designed the first commercial small satellite CMGs currently in orbit on the Turkish BILSAT-1 microsatellite. This project was funded by SSTL, ESA and the Turkish Academy of Sciences (TUBITAK). Under funding from ESA Vaios is leading the design of an improved and scalable CMG design for small satellites. Vaios is working closely with Prof. Bong Wie on the development of these CMGs along with various singularity avoidance algorithms.
Solar Sails
Solar Sails have become one the ‘hottest topics’ in the space community and specifically in the systems design and attitude control aspects. Solar Sails come with the promise of propelling spacecraft with unprecedented ΔVs without ‘propellant’. Solar Sails work as protons reflect on a large reflector surface. Vaios has been the PI and study manager for a miniature 5 x 5 m micro sail for a study funded by ESA. Micro Solar Sails come with the promise of low cost propellantless systems that do not have the technology challenges of large solar sails (design, dynamics, control, manufacture) and can be used in formations to study niche science objectives such as monitoring the Earth’s geomagnetic tail. On the other spectrum Vaios participated in an ESA funded studied managed by Kayser Threde and dealt with the conceptual design of a 245 x 245 m solar sail called the Interstellar Heliopause Probe (IHP). Surrey was responsible for the small satellite platform design and the overall spacecraft/sail GNC system. Vaios is also working closely together with Prof. Bong Wie on various systems and ACS concepts for Solar Sails.
Combined Energy Storage and Attitude Control Systems (CEACS)
CEACS comes with the promise of reducing the mass of a spacecraft, which has high power and ACS requirements. Vaios is the PI on a USAF contract which is studing the sizing, design and proof of concept of such technology for small satellites. Further, Vaios with his PhD student David Richie are working on the same research contract for the USAF on studying various control algorithms for a large scale CEACS system developed by the USAF in the Air Force Research Laboratories in Kirkland, NM, USA.
UAV’s
Unmanned Aerial Vehicles have become important tools for reconnaissance and robotic missions. Vaios is researching systems and algorithms for autonomous systems using a 3-m UAV helicopter. The ‘ICARUS’ vehicle will also be used to demonstrate robust algorithms for terminal descent Mars Lander simulations.
Mars Landers and Mars Ascent Vehicles
Vaios has worked on the system design and GNC algorithms for Mars landers and ascent vehicles with MSc and PhD students. This research was funded by the ESA Aurora program.
Spacecraft Simulator
Space engineering despite progress made in low cost design is still and expensive and complex business. A spacecraft simulator based on a 3-axis air bearing is being designed at Surrey. George Prassinos is leading this effort which will include propulsion and CMG modules for agile 3-axis control.
1-m Resolution Small Satellites
Funded by SSTL this research activity explores the technological shortcomings on developing the next generation of 1-m resolution Earth Observation spacecraft. Based on the known concept of the Dobson telescope Surrey is studying the technology for future use. George Prassinos is currently conducting his MPhil on this subject.
Formation Flying/Coulomb and Lorentz Formations
Surrey and Cornell Universities are working together on a research grant by ESA ACT (Ariadna) on formation flying missions using Lorentz and Coulomb charging techniques. Mini Saaj, a research fellow from Surrey is actively working on a hybrid combination of the two techniques under supervision by Vaios and Mason Peck, Assistant Professor, Cornell University.
Propulsion
Propulsion is a key research area at Surrey. Micro-resistojet thrusters have been mastered at Surrey, many of them having flown on UoSAT-12, SNAP and DMC spacecraft. Vaios is supervising two PhD students on electric propulsion: Peter Shaw working on Plasma Pulsed Thrusters and Angelo Grubisic working on micro hollow cathode tubes.
Research Collaborations
Vaios work closely with Prof. Bong Wie (Arizona State University), Mason Peck (Cornell), Prof. Jozef van der Ha (consultant), Prof. N. Uzunoglou (NTUA), Prof. E. Sarris (Democritus-Thrace) and Jerry Fausz (USAF). Internally Vaios works with all academics in SSC and is assisting Dr. Craig Underwood on the Palmsat program.
Publications
Highlights
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(2009) 'Robust Control Moment Gyroscope Steering Logic with Gimbal Angle Constraints'. AMER INST AERONAUT ASTRONAUT JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, Keystone, CO: 32 (5), pp. 1662-1666.doi: 10.2514/1.43806
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(2009) 'Practical Systems Design for an Earth-Magnetotail-Monitoring Solar Sail Mission'. AMER INST AERONAUT ASTRONAUT J SPACECRAFT ROCKETS, 46 (2), pp. 381-393.doi: 10.2514/1.32040
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(2009) 'Survey of Technology Developments in Flywheel Attitude Control and Energy Storage Systems'. AMER INST AERONAUT ASTRONAUT JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 32 (2), pp. 354-365.doi: 10.2514/1.32092
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(2009) 'Practical steering law for small satellite energy storage and attitude control'. Journal of Guidance, Control, and Dynamics, 32 (6), pp. 1898-1911.doi: 10.2514/1.41968
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(2009) 'Redundant reaction wheel torque distribution yielding instantaneous L 2 power-optimal attitude control'. Journal of Guidance, Control, and Dynamics, 32 (4), pp. 1269-1276.doi: 10.2514/1.41070
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(2007) 'Microsolar sails for Earth magnetotail monitoring'. AMER INST AERONAUT ASTRONAUT JOURNAL OF SPACECRAFT AND ROCKETS, 44 (4), pp. 840-848.doi: 10.2514/1.23456
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(2006) 'Wireless sensor motes for small satellite applications'. IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC IEEE ANTENNAS AND PROPAGATION MAGAZINE, 48 (5), pp. 175-179.Full text is available at: http://epubs.surrey.ac.uk/62/
- . (2006) 'Robust CMG steering logic with gimbal angle constraints'. Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, 2, pp. 1425-1438.
Journal articles
- . (2012) 'Architecture and systems design of a reusable Martian twin rotor tailsitter'. Acta Astronautica, 80, pp. 166-180.
- . (2012) 'The European Union funded NEOShield project: A global approach to near-Earth object impact threat mitigation'. Acta Astronautica,
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(2011) 'Direct thrust measurement of a permanent magnet helicon double layer thruster'. AMER INST PHYSICS APPLIED PHYSICS LETTERS, 98 (14) Article number ARTN 141503 doi: 10.1063/1.3577608
- . (2011) 'Exploration of Lunar Craters Using a Tracked Microrover Concept for the ESA Lunar Robotics Challenge'. British interplanetary Society Journal of British Interplanetary Society, UK: 63 (7), pp. 267-277.
- . (2011) 'Completely stripped solar sail concept using bi-stable reeled composite booms'. Acta Astronautica, 69 (1-2), pp. 78-85.
- . (2011) 'Completely stripped solar sail concept using bi-stable reeled composite booms'. Acta Astronautica,
- . (2011) 'Cubesat solar sail 3-axis stabilization using panel translation and magnetic torquing'. Aerospace Science and Technology,
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(2010) 'Erratum: Survey of technology developments in flywheel attitude control and energy storage systems (Journal of Guidance, Control, and Dynamics (2009) 32:2 (354-365))'. Journal of Guidance, Control, and Dynamics, 33 (1), pp. 286-286.doi: 10.2514/1.47362
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(2010) 'Survey of Technology Developments in Flywheel Attitude Control and Energy Storage Systems (vol 32, pg 354, 2009)'. AMER INST AERONAUT ASTRONAUT JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 33 (1), pp. 286-286.doi: 10.2514/1.47362
- . (2010) 'Hybrid propulsion system for formation flying using electrostatic forces'. ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER AEROSPACE SCIENCE AND TECHNOLOGY, 14 (5), pp. 348-355.
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(2009) 'Robust Control Moment Gyroscope Steering Logic with Gimbal Angle Constraints'. AMER INST AERONAUT ASTRONAUT JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, Keystone, CO: 32 (5), pp. 1662-1666.doi: 10.2514/1.43806
- .
(2009) 'Practical Systems Design for an Earth-Magnetotail-Monitoring Solar Sail Mission'. AMER INST AERONAUT ASTRONAUT J SPACECRAFT ROCKETS, 46 (2), pp. 381-393.doi: 10.2514/1.32040
- .
(2009) 'Survey of Technology Developments in Flywheel Attitude Control and Energy Storage Systems'. AMER INST AERONAUT ASTRONAUT JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 32 (2), pp. 354-365.doi: 10.2514/1.32092
- .
(2009) 'Practical steering law for small satellite energy storage and attitude control'. Journal of Guidance, Control, and Dynamics, 32 (6), pp. 1898-1911.doi: 10.2514/1.41968
- . (2009) 'A practical small satellite variable-speed control moment gyroscope for combined energy storage and attitude control'. Acta Astronautica, 65 (11-12), pp. 1745-1764.
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(2009) 'Redundant reaction wheel torque distribution yielding instantaneous L 2 power-optimal attitude control'. Journal of Guidance, Control, and Dynamics, 32 (4), pp. 1269-1276.doi: 10.2514/1.41070
- .
(2007) 'Microsolar sails for Earth magnetotail monitoring'. AMER INST AERONAUT ASTRONAUT JOURNAL OF SPACECRAFT AND ROCKETS, 44 (4), pp. 840-848.doi: 10.2514/1.23456
- . (2007) 'Hybrid propulsion system for spacecraft swarm aggregation using Coulomb force'. BRITISH INTERPLANETARY SOC JBIS-JOURNAL OF THE BRITISH INTERPLANETARY SOCIETY, 60 (7), pp. 268-274.
- . (2007) 'Spacecraft formation flying using Lorentz forces'. BRITISH INTERPLANETARY SOC JBIS-JOURNAL OF THE BRITISH INTERPLANETARY SOCIETY, 60 (7), pp. 263-267.
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(2007) 'Sizing/optimization of a small satellite energy storage and attitude control system'. AMER INST AERONAUT ASTRONAUT JOURNAL OF SPACECRAFT AND ROCKETS, 44 (4), pp. 940-952.doi: 10.2514/1.25134
- . (2007) 'Spacecraft formation flying and reconfiguration with electrostatic forces'. AMER ASTRONAUTICAL SOC SPACE FLIGHT MECHANICS 2007, VOL 127, PTS 1 AND 2, Sedona, AZ: 127, pp. 217-225.
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(2007) 'Long-term attitude drift of spinning spacecraft under solar radiation torques'. Journal of Guidance, Control, and Dynamics, 30 (5), pp. 1470-1479.doi: 10.2514/1.28506
- . (2007) 'Saving mass in optimally sizing a small satellite energy storage and attitude control system'. Advances in the Astronautical Sciences, 127 PART 2, pp. 1161-1177.
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(2007) 'Optimal steering law for the GeoSail mission'. Journal of Guidance, Control, and Dynamics, 30 (3), pp. 876-879.doi: 10.2514/1.28765
- . (2007) 'Combined singularity avoidance for variable speed control moment gyroscope clusters'. Advances in the Astronautical Sciences, 127 PART 2, pp. 1213-1224.
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(2006) 'Wireless sensor motes for small satellite applications'. IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC IEEE ANTENNAS AND PROPAGATION MAGAZINE, 48 (5), pp. 175-179.Full text is available at: http://epubs.surrey.ac.uk/62/
- . (2006) 'Solar kites for earth magneto-tail monitoring'. ESA PUBLICATIONS DIVISION C/O ESTEC First Workshop on Innovative System Concepts, Proceedings, Noordwijk, NETHERLANDS: 633, pp. 73-80.
- . (2006) 'Agile maneuvers for near earth object (NEO) fly-by missions'. ESA PUBLICATIONS DIVISION C/O ESTEC FIRST WORKSHOP ON INNOVATIVE SYSTEM CONCEPTS, PROCEEDINGS, Noordwijk, NETHERLANDS: 633, pp. 65-72.
- . (2006) 'Long-term attitude drift of spinning spacecraft under solar radiation torques'. Advances in the Astronautical Sciences, 123 II, pp. 1123-1142.
- . (2006) 'Attitude control design for solar sail missions'. European Space Agency, (Special Publication) ESA SP, (606), pp. 191-194.
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(2006) 'Spacecraft swarm navigation and control using artificial potential field and sliding mode control'. IEEE 2006 IEEE International Conference on Industrial Technology, Vols 1-6, Bombay, INDIA: , pp. 2809-2814.Full text is available at: http://epubs.surrey.ac.uk/2276/
- . (2006) 'Autonomous attitude determination and control for low-cost deep space probes'. European Space Agency, (Special Publication) ESA SP, (606), pp. 269-278.
- . (2006) 'Systems design for a 1-M resolution small satellite earth observation mission'. AIAA 57th International Astronautical Congress, IAC 2006, 4, pp. 2323-2331.
Conference papers
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(2011) 'STRaND-1: Use of a $500 Smartphone as the Central Avionics of a Nanosatellite'. International Astronautical Federation Proceedings of the 2nd International Astronautical Congress 2011, (IAC ’11), Cape Town, South Africa: 62nd International Astronautical Congress 2011, (IAC ’11)Full text is available at: http://epubs.surrey.ac.uk/26828/
Abstract
STRaND-1 is the first in a series of Surrey Satellite Technology Ltd. (SSTL)-Surrey Space Centre (SSC) collaborative satellites designed for the purpose of technology path finding for future commercial operations. It is the first time Surrey has entered the CubeSat field and differs from most CubeSats in that it will fly a modern Commercial Off The Shelf (COTS) Android smartphone as a payload, along with a suite of advanced technologies developed by the University of Surrey, and a payload from the University of Stellenbosch in South Africa. STRaND- 1 is also different in that anyone (not just from the space engineering or space science community) will be eligible to fly their “app" in space, for free. STRaND-1 is currently being manufactured and tested by volunteers in their own free time, and will be ready for an intended launch in the first quarter of 2012. This paper outlines the STRaND pathfinder programme philosophy which challenges some conventional space engineering practises, and describes the impact of those changes on the satellite development lifecycle. The paper then briefly describes the intent behind the design of STRaND-1, before presenting details on the design of the nanosatellite, focussing of the details of the innovative new technologies. These technologies include two different propulsion systems, an 802.11g WiFi experiment, a new VHF/UHF transceiver unit and a miniature 3-axis reaction wheel assembly. The novel processing setup (which includes the smartphone) is discussed in some detail, particularly the potential for outreach via the open source nature of Google's Android operating system. A stepthrough of the planned concept of operations is provided, which includes a possible rendezvous and inspection objective, demonstrating equal or improved capability compared to SNAP-1 with a reduced total system mass. Finally, data from the test campaign is presented and compared against other notable CubeSats known for their advanced capabilities. Rendered images of STRaND-1 are shown in Fig. I and are discussed later in the paper.
- . (2011) 'STRaND-1: The world's first smartphone nanosatellite'. 2nd International Conference on Space Technology, ICST 2011,
- . (2008) 'A practical small satellite variable-speed control moment yroscope for combined energy storage and attitude control'. AIAA/AAS Astrodynamics Specialist Conference and Exhibit,
- . (2008) 'Scalable bus-based attitude control system for solar sails'. International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008, 8, pp. 5215-5222.
- . (2008) 'A practical variable-speed control moment gyroscope steering law for small satellite energy storage and attitude control'. AIAA/AAS Astrodynamics Specialist Conference and Exhibit,
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(2007) 'Characterising wireless sensor motes for space applications'. IEEE COMPUTER SOC NASA/ESA Conference on Adaptive Hardware and Systems, Proceedings, Univ Edinburgh, Edinburgh, SCOTLAND: 2nd NASA/ESA Conference on Adaptive Hardware and Systems, pp. 43-50.Full text is available at: http://epubs.surrey.ac.uk/2002/
- . (2006) 'Prometheus: A low-cost microsatellite flyby mission of 4179 Toutatis'. PERGAMON-ELSEVIER SCIENCE LTD ACTA ASTRONAUTICA, European Space Res & Technol Ctr, Noordwijk, NETHERLANDS: 5th IAA International Conference on Low-Cost Planetary Missions 59 (8-11), pp. 834-844.
- . (2006) 'Advanced satellite bus technology for near-term solar sail missions'. Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, 1, pp. 570-588.
- . (2006) 'Micro CMGs for agile small satellites: Design and in-orbit tests'. European Space Agency, (Special Publication) ESA SP, (606), pp. 667-675.
- . (2006) 'Robust CMG steering logic with gimbal angle constraints'. Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, 2, pp. 1425-1438.
- . (2006) 'Mathematical modeling of high effeciency pulsed plasma thrusters for microsatellites'. AIAA 57th International Astronautical Congress, IAC 2006, 10, pp. 6681-6693.
- . (2006) 'Utilising the EyasSAT concept in space systems engineering courses at the University of Surrey'. AIAA 57th International Astronautical Congress, IAC 2006, 13, pp. 9070-9083.
Teaching
Vaios teaches undergraduate and postgraduate courses in the School of Electronics. These include Spacecraft Dynamics and Control (EE3.dyc), Launch Vehicles and Propulsion (EEM.lvp), Satellite Subsystems (EE3.sbs) and Control Engineering (EE3.ctl). Vaios also supervises undergraduate and postgraduate students in topics such as: attitude control, micro UAVs, Mars Lander dynamics and control, solar sail attitude control.
PhD Students
Vaios is currently supervising 3 PhD students: Peter Shaw on PPTs, Angelo Grubisic on micro-HCT, David Richie on CEACS, Alice Darbyshire on CMGs and he also has worked with Sajjad Ashgar (CMGs) and Stephen Wokes (solar sails) who are supervised by Dr. Palmer and Prof. Mark Roberts.
Awards
- AIAA Utah Small Satellite Student Competition (3rd Place), 2000
- IAF Student Competition (1st place) 2001
- Canadian Space Agency Caroline Babin award (2000)
- Best paper, co-author with Jozef van der Ha, AAS Astrodynamics Specialist Conference (lake tahoe), 2006
- Scholaships: EUMETSAT, SSTL, EPSRC, Canadian Space Agency, ESA
- Grants (royal Society, UniS, Institute for Advanced Studies)
Consulting
- Vaios consults for the Hellenic Space Systems company.
