Initial design of flight data acquisition unit (FDAU)

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:International Seminar of Aerospace Science and Technology (7. : 2019 : Jakarta) 7th International Seminar on Aerospace Science and Technology - ISAST 2019
1. Verfasser: Wardana, Try Kusuma (VerfasserIn)
Weitere Verfasser: Pranoto, Fuad Surastyo (VerfasserIn), Bahri, Sayr (VerfasserIn), Suseno, Prasetyo Ardi Probo (VerfasserIn), Bintoro, Atik (VerfasserIn)
Pages:7
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2020
Schlagworte:
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Titel Jahr Verfasser
Analysis of aerodynamic characteristics using the vortex lattice method on twin tail boom unmanned aircraft 2020 Septiyana, A.
Mathematical modeling of LAPAN surveillance UAV (LSU) — 02 for automatic control and guidance system design 2020 Fathurrahman, A.
Mathematical modelling and simulation of a quadrotor unmanned aerial vehicle with automatic altitude and speed control 2020 Jenie, Y. I.
Initial design of flight data acquisition unit (FDAU) 2020 Wardana, Try Kusuma
Power control system for the RX-320 atmospheric payload sounding rocket 2020 Artono, Endro
Centralized swarming UAV using ROS for collaborative missions 2020 Indriyanto, T.
Thrust modelling for a small UAV 2020 Safi'i, I.
Finite element modeling and analysis of heat transfer in a 122-mm diameter solid rocket nozzle 2020 Gantina, Hendra
Experimental investigation on crashworthiness characteristics of e-glass-lycal composite tube and local product aluminum tube using quasi-static crushing test 2020 Hidayat, Dony
Analysis of composite propellant energy and correlation with specific impulse at vacuum level 2020 Prianto, B.
Numerical analysis of vena contracta orifice for liquid rocket engine LAPAN feed system 2020 Yusuf, N. R.
Further development of low cost thrust benchmarking system (TBS) for dynamic thrust measurement 2020 Ramadhani, M. J.
Energy consumption comparison of static pitch propeller and variable pitch propeller using maximum thrust equation approach in small scale electric unmanned aerial vehicle 2020 Stevenson, R.
Computational fluid dynamics based winglet design and analysis of GL-1 glider 2020 Moelyadi, M. A.
Full envelope six-degree of freedom simulation of tactical missile 2020 Wibowo, S. S.
Design and CFD simulation of a compact supersonic wind tunnel 2020 Moelyadi, M. A.
Experimental flight control function for electronic flight control system of high aspect ratio light utility aircraft 2020 Suseno, P. A. P.
Analysis of GPS antenna visibility for rocket using SDR 2020 Widada, Wahyu
Preliminary design of MYSat payload: Electron temperature and density probe (TeNeP) generator circuit 2020 Latif, M. A. A.
A new data communication protocol for rocket and UAV with improved efficiency and capabilities 2020 Irwanto, H. Y.
Alle Artikel auflisten