Browse by Journal Title

Aslam, Sohaib and Yew, Chung Chak and Jaffery, Mujtaba Hussain and Varatharajoo, Renuganth (2022) The fuzzy PD control for combined energy and attitude control system. Aircraft Engineering and Aerospace Technology, 94 (10). 1806 - 1824. ISSN 0002-2667

Aw, Aaron Teik Hong and Varatharajoo, Renuganth and Romli, Fairuz Izzudin (2015) Analytic solutions for Tethered Satellite System (TSS) subject to internal and external torques undergoing a spin-up and spin-down maneuvers. Aircraft Engineering and Aerospace Technology, 87 (6). pp. 514-520. ISSN 0002-2667

Abdullah, Mohammad Nizam Filipski and Varatharajoo, Renuganth (2010) Evaluation of a spacecraft attitude and rate estimation algorithm. Aircraft Engineering and Aerospace Technology, 82 (3). pp. 184-193. ISSN 1748-8842; ESSN: 1758-4213

Djojodihardjo, Harijono and Ahmed, Riyadh Ibraheem and Abu Talib, Abd Rahim and Mohd Rafie, Azmin Shakrine (2017) First principle analysis of Coandă Micro Air Vehicle aerodynamic forces for preliminary sizing. Aircraft Engineering and Aerospace Technology, 89 (2). pp. 231-245. ISSN 1748-8842; ESSN: 1758-4213

Ismail, Zuliana and Varatharajoo, Renuganth and Mohd Ajir, Mohd Ramly and Mohd Rafie, Azmin Shakrine (2015) Enhanced attitude control structure for small satellites with reaction wheels. Aircraft Engineering and Aerospace Technology, 87 (6). pp. 546-550. ISSN 748-8842; ESSN: 1758-4213

Romli, Fairuz Izzudin and Harmin, Mohammad Yazdi (2015) Use of Monte Carlo method to estimate subsystem redesign risk for complex products: aircraft redesign case study. Aircraft Engineering and Aerospace Technology, 87 (6). pp. 563-570. ISSN 1748-8842; ESSN: 1758-4213

Salleh, Mohd Badrul and Mohd Suhadis, Nurulasikin and Varatharajoo, Renuganth (2021) An active force controlled of small CMG-based satellite. Aircraft Engineering and Aerospace Technology, 93 (7). 1183 - 1192. ISSN 1748-8842; ESSN: 1758-4213

Yew, Chung Chak and Varatharajoo, Renuganth (2015) A novel design of spacecraft combined attitude & sun tracking system using a versatile fuzzy controller. Aircraft Engineering and Aerospace Technology, 87 (6). pp. 530-539. ISSN 0002-2667