Optimal geometric motion planning for a spin-stabilized spacecraft JD Biggs, N Horri Systems & Control Letters 61 (4), 609-616, 2012 | 162 | 2012 |
Practical implementation of attitude-control algorithms for an underactuated satellite NM Horri, P Palmer Journal of Guidance, Control, and Dynamics 35 (1), 40-45, 2012 | 102 | 2012 |
Attitude stabilization of an underactuated satellite using two wheels N Horri, S Hodgart IEEE Aerospace conference, 2629-2635, 2003 | 74 | 2003 |
Gain-scheduled inverse optimal satellite attitude control NM Horri, P Palmer, M Roberts IEEE Transactions on aerospace and electronic systems 48 (3), 2437-2457, 2012 | 38 | 2012 |
STRaND-2: Visual inspection, proximity operations & nanosatellite docking CP Bridges, B Taylor, N Horri, CI Underwood, S Kenyon, J Barrera-Ars, ... 2013 IEEE Aerospace Conference, 1-8, 2013 | 33 | 2013 |
Autonomous assembly of a reconfiguarble space telescope (aarest)–a cubesat/microsatellite based technology demonstrator C Underwood, S Pellegrino, V Lappas, C Bridges, B Taylor, S Chhaniyara, ... | 33 | 2013 |
Relative attitude dynamics and control for a satellite inspection mission NM Horri, KU Kristiansen, P Palmer, M Roberts Acta Astronautica 71, 109-118, 2012 | 22 | 2012 |
A tutorial and review on flight control co-simulation using matlab/simulink and flight simulators N Horri, M Pietraszko Automation 3 (3), 486-510, 2022 | 19 | 2022 |
Energy optimal spacecraft attitude control subject to convergence rate constraints NM Horri, PL Palmer, M Roberts Control Engineering Practice 19 (11), 1297-1314, 2011 | 19 | 2011 |
A box regularized particle filter for state estimation with severely ambiguous and non-linear measurements N Merlinge, K Dahia, H Piet-Lahanier, J Brusey, N Horri Automatica 104, 102-110, 2019 | 17 | 2019 |
Investigation of a mission-based sizing method for electric VTOL aircraft preliminary design O Ugwueze, T Statheros, N Horri, M Innocente, M Bromfield AIAA Scitech 2022 Forum, 1931, 2022 | 16 | 2022 |
Tilted wheel satellite attitude control with air-bearing table experimental results LO Inumoh, JL Forshaw, NM Horri Acta Astronautica 117, 414-429, 2015 | 15 | 2015 |
An Efficient and Robust Sizing Method for eVTOL Aircraft Configurations in Conceptual Design O Ugwueze, T Statheros, N Horri, MA Bromfield, J Simo Aerospace 10 (3), 311, 2023 | 12 | 2023 |
Bounded gain-scheduled LQR satellite control using a tilted wheel LO Inumoh, NM Horri, JL Forshaw, A Pechev IEEE Transactions on Aerospace and Electronic Systems 50 (3), 1726-1738, 2014 | 12 | 2014 |
Optimal satellite attitude control: A geometric approach NM Horri, PL Palmer, MR Roberts 2009 IEEE Aerospace conference, 1-11, 2009 | 11 | 2009 |
Trends in eVTOL aircraft development: the concepts, enablers and challenges O Ugwueze, T Statheros, MA Bromfield, N Horri AIAA Scitech 2023 forum, 2096, 2023 | 9 | 2023 |
Autonomous Assembly of a Reconfigurable Space Telescope (AAReST)-Rendezvous and docking on a 2D test-bed C Underwood, S Pellegrino, B Taylor, S Chhaniyara, N Horri 9th IAA Symposium on Small Satellites for Earth Observation, IAA-B9-0508, 2013 | 7 | 2013 |
Design and validation of inverse optimisation software for the attitude control of microsatellites NM Horri, P Palmer, M Roberts Acta Astronautica 69 (11-12), 997-1006, 2011 | 7 | 2011 |
Attitude control of underactuated small satellites NM Horri PQDT-Global, 2004 | 7 | 2004 |
Three-axis attitude control of a satellite in zero momentum mode using a tilted wheel methodology L Inumoh, A Pechev, N Horri, J Forshaw AIAA Guidance, Navigation, and Control Conference, 4752, 2012 | 6 | 2012 |