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20072022
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Research Output 2007 2018

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Conference contribution book
2017

Conceptual design analysis for a two-stage-to-orbit semi-reusable launch system for small satellites

Maddock, C., Toso, F., West, M., West, J., Kontis, K., Rengarajan, S., Evans, D., Milne, A. & McIntyre, S., 25 Sep 2017, 68th Proceedings of the International Astronautical Congress. Adelaide, South Australia, 14 p. IAC-17-D2.7.12

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

Open Access
File
Conceptual design
Orbits
Satellites
Aircraft carriers
Launch vehicles

Return and abort trajectory optimisation for reusable launch vehicles

Toso, F. & Maddock, C., 2 Mar 2017, Proceedings of the 21st AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston, VA, 11 p. AIAA 2017-2250. (International Space Planes and Hypersonic Systems and Technologies Conferences).

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

Open Access
File
Launch vehicles
Trajectories
Recovery
2 Citations (Scopus)

Vehicle and mission design of a future small payload launcher

Maddock, C. A., Toso, F., Ricciardi, L., Mogavero, A., Lo, K. H., Rengarajan, S., Kontis, K., Milne, A., Merrifield, J., Evans, D., West, M. & McIntyre, S., 2 Mar 2017, 21st AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston, VA, 21 p. AIAA 2017-2224. (International Space Planes and Hypersonic Systems and Technologies Conferences).

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

Open Access
File
Aircraft carriers
Launch vehicles
Conceptual design
Orbits
Earth (planet)
2016
2 Citations (Scopus)

Global solution of multi-objective optimal control problems with multi agent collaborative search and direct finite elements transcription

Ricciardi, L. A., Vasile, M. & Maddock, C., 21 Nov 2016, 2016 IEEE Congress on Evolutionary Computation, (CEC). Piscataway: IEEE, p. 869-876 8 p. 7743882

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

Open Access
File
Transcription
Global Solution
Optimal Control Problem
Finite Element
Nonlinear programming
2 Citations (Scopus)

Multi-objective optimal control of ascent trajectories for launch vehicles

Ricciardi, L. A., Vasile, M., Toso, F. & Maddock, C. A., 13 Sep 2016, AIAA/AAS Astrodynamics Specialist Conference, 2016. Reston, VA, 14 p. 2016-5669. (AIAA Space Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

Open Access
File
ascent trajectories
launch vehicles
Launch vehicles
optimal control
Trajectories

Spaceplane trajectory optimisation with evolutionary-based initialisation

Maddock, C. & Minisci, E., 9 Dec 2016, Proceedings of the IEEE Symposium Series on Computational Intelligence. Piscataway: IEEE, 8 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

Open Access
File
Propulsion
Trajectories
Transcription
Rockets
Orbits
2010
1 Citation (Scopus)

Integrated 915 MHz dual-patch circularly polarized antenna for Suaineadh space web experiment

Whyte, G., Murray, C., Maddock, C., Vasile, M. & Drysdale, T. D., 11 Jul 2010, Proceedings of the IEEE Symposium on Antennas and Propagation: CNC/USNC/URSI Radio Science Meeting. IEEE, p. 1-4 5 p. (Antennas and Propagation).

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

Rockets
Microstrip antennas
Patch
Antenna
Antennas