Follow
Taufiq Mulyanto
Taufiq Mulyanto
Faculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung
Verified email at ae.itb.ac.id - Homepage
Title
Cited by
Cited by
Year
Utilisation des techniques de programmation par contraintes pour la conception d'avions
T Mulyanto
École nationale supérieure de l'aéronautique et de l'espace (Toulouse; 1972 …, 2002
252002
Path following system of small unmanned autonomous vehicle for surveillance application
RA Sasongko, J Sembiring, H Muhammad, T Mulyanto
2011 8th Asian Control Conference (ASCC), 1259-1264, 2011
162011
Total least squares estimation of aerodynamic parameter of micro coaxial helicopter from flight data
H Muhammad, HP Thien, T Mulyanto
Int. J. Basic Appl. Sci 12 (2), 44-52, 2012
112012
Comparative study between Schrenk and CFD analysis for predicting lift distribution along wing span of glider aircraft
CA Putra, R Julistina, MA Moelyadi, T Mulyanto
Advance in Aerospace Science and Technology in Indonesia 1, 108-117, 2016
92016
A generic approach for conceptual design based on object oriented and constraint logic programming
E Bensana, T Mulyanto
International conference on engineering design and automation, Orlando, Floride, 2000
82000
The development of an autonomous control system for a small UAV: Waypoints following system
RA Sasongko, T Mulyanto, AH Wijaya
2009 7th Asian Control Conference, 308-313, 2009
72009
Glider uncentered drag polar estimation based on flight manual data
NAD Kurniasari, MLI Nurhakim, O Arifianto, T Mulyanto
Advance in Aerospace Science and Technology in Indonesia 1, 118-125, 2016
62016
Flight test of GL-1 glider half scale prototype
MF Zulkarnain, MF Rahman, MLI Nurhakim, O Arifianto, T Mulyanto
Journal of Physics: Conference Series 1005 (1), 012031, 2018
42018
Conceptual design of blended wing body business jet aircraft
T Mulyanto, M Luthfi Imam Nurhakim
Journal of KONES 20 (4), 299-306, 2013
42013
Mathematical modeling and experimental identification of micro coaxial helicopter dynamics
HP Thien, T Mulyanto, H Muhammad, S Suzuki
International Journal of Basic & Applied Sciences 12 (2), 353-364, 2012
42012
Mathematical modeling, simulation and identification of micro coaxial helicopter
H Muhammad, HP Thien, T Mulyanto
Journal of KONES 19, 353-364, 2012
42012
Dealing with uncertainty in design and configuration problems
E Bensana, T Mulyanto, G Verfaillie
Configuration, 13, 2000
42000
Preliminary design of GL-1 sailplane cockpit arrangement and control mechanism based on EASA CS-22 requirements
T Mulyanto, MF Zulkarnain
IOP Conference Series: Materials Science and Engineering 645 (1), 012005, 2019
32019
Development of pose estimation system based on dual camera techniques for parameter identification of indoor MAV
T Mulyanto, MLI Nurhakim, H Muhammad
Proc. 28th Int. Congr. of the Aeronautical Sciences (ICAS), Brisbane, 2012
32012
Conception, Configuration et Incertitude dans le cadre de la Programmation par Contraintes
T Mulyanto
5èmes Rencontres Jeunes Chercheurs en Intelligence Artificielle, Lyon, 2000
32000
Estimation of Lateral/Directional Static Stability Characteristics of a Turboprop Aircraft at One Engine Inoperative Condition
RA Wandini, T Mulyanto, H Muhammad
Applied Mechanics and Materials 842, 208-216, 2016
22016
Dynamic Modeling and Control System Development of a Coaxial Rotor MAV
HP Thien, T Mulyanto, H Muhammad
International Forum on Strategic Technologies, 118-123, 2009
22009
From document-based to model-based systems engineering, case studies of BRIN LSA-02 electronic flight control systems
AM Pramutadi, MF Zulkarnain, T Mulyanto, IP Nurprasetio
AIP Conference Proceedings 2941 (1), 2023
12023
Computational fluid dynamics analysis and aircraft performance studies of GL-1’s spoiler extension
T Mulyanto, MF Zulkarnain
AIP Conference Proceedings 2366 (1), 2021
12021
Indonesian glider GL-1 spoiler preliminary design and computational fluid dynamics analysis using EASA CS-22 performance requirements
T Mulyanto, MF Zulkarnain
IOP Conference Series: Materials Science and Engineering 1173 (1), 012048, 2021
12021
The system can't perform the operation now. Try again later.
Articles 1–20