PEMBUATAN DAN PENGUJIAN SENSOR ULTRASONIK SEBAGAI FEEDBACK PADA SISTEM KENDALI OTOMATIK PITCH ATTITUDE HOLD
Abstract
Standard altimeter, i.e. static tube, does not work accurate enough for vehicle flying several meters from the ground. One alternative for measuring altitude in this case is using ultrasonic range-meter. This idea is brought further by using two range-meters to measure pitch attitude. Laboratory experiments were conducted to study this idea statically by constructing them in an inclined moving bar and dynamically by arranging them in a Pitch Attitude Hold control system.
References
U.M. Zaeny, Pembuatan dan Pengujian Sensor
Ultrasonik sebagai Feedback pada Sistem Kendali
Otomatik Pitch Attitude Hold, Thesis, Teknik
Penerbangan ITB, 2006.
M.N. Syaefullah, Perancangan dan Implemen-tasi
Proximity Meter Berbasis Mikrokontroler
At89c2051, Tugas Akhir, Fisika, FMIPA ITB, 2003.
http://www.interq.or.jp/japan/se-inoue/esrm.htm,
Circuit explanation of Ultrasonic Range Meter Unit,
Maret 2003.
A.E. Putro, Belajar Mikrokontroler AT89C51/52/ 55
Teori dan Aplikasi, Gava Media Yogyakarta, 2000.
E. Kreyzig, Advanced Engineering Mathematics, 8th
Edition, John Wiley & Son Inc, 1999.
S.D. Jenie, Catatan Kuliah Teknik Kendali Terbang
, Teknik Penerbangan, ITB, 1991.


