ALTITUDE CONTROL SYSTEM OF UCAV WITH TOTAL ENERGY CONTROL SYSTEM
<p align="justify">UCAV (Unmanned Combat Aerial Vehicle) is an unmanned flying vehicle designed to carry out combat missions. UCAV must have high efficiency to be able to carry out specific missions and maneuvers. In the profile of the UAV mission there is a cruise mission, at this t...
Saved in:
Main Author: | Nuriwati - NIM : 13614031 , Rika |
---|---|
Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/30487 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
ATTITUDE AND FLIGHT PATH CONTROL SYSTEM OF UNMANNED COMBAT AERIAL VEHICLE (UCAV)
by: Hanif - Nim: 13614007 , Azizul -
AUTOMATIC COLLISION AVOIDANCE SYSTEM ON UCAV
by: Faris Shahab, Ahmad -
DEVELOPMENT AND HARDWARE IN-THE-LOOP IMPLEMENTATION OF TOTAL ENERGY CONTROL SYSTEM FOR ALTITUDE CONTROL OF A SCALED DOWN (1:2) MODEL OF ITB HALE UAV
by: Ariyanto, Jordy -
MULTIMODE FLIGHT CONTROL SYSTEM OF UNMANNED COMBAT AERIAL VEHICLE (UCAV) USING EIGENSTRUCTURE ASSIGNMENT METHOD
by: Valmay Priyono, Aathirah -
MANEUVER CONTROL OF UNMANNED COMBATANT AERIAL VEHICLE (UCAV) USING UNCONVENTIONAL EFFECTOR
by: Ekananto, Rayhan