PRELIMINARY DESIGN AND SAFETY ASSESSMENT OF WIRELESS FLIGHT CONTROL SYSTEM: AE301 AIRPLANE CASE STUDY
Sistem kendali terbang merupakan sistem yang penting bagi pesawat udara. Berbagai teknologi dikembangkan untuk meningkatkan keandalan dan mengurangi kontribusi berat dari system ini ke pesawat udara. Dalam penelitian ini akan dipelajari kelayakan penggunaan teknologi nirkabel untuk dapat diterapkan...
Saved in:
Main Author: | Hardyan Prasetya, Oldhi |
---|---|
Format: | Theses |
Language: | Indonesia |
Subjects: | |
Online Access: | https://digilib.itb.ac.id/gdl/view/47412 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM
by: Iman Effendi, Nurul -
DETECTION MODELLING OF AIRPLANE BLACK BOX USING RAY TRACING METHOD IN MAKASSAR STRAIT
by: Ruth Angie Manurung, Honey -
QUANTIFICATION OF CONTROLLED FLIGHT INTO TERRAIN ACCIDENT PROBABILITY BASED ON FLIGHT OPERATIONAL DATA
by: Aulia Soegiharto, Fikri -
FLIGHT DYNAMIC MODELLING AND STUDY ON THE IMPLEMENTATION OF FLIGHT CONTROL SYSTEM OF EXPERIMENTAL FIGHTER AIRCRAFT FXX
by: Kus Wardana, Yustinus -
COMPUTATIONAL AERODYNAMICS AND FLIGHT SIMULATION BASED FLIGHT TEST PLAN DESIGN FOR UNMANNED AERIAL VEHICLE
by: Akhdiyatullah G., Syahrahman