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All Journal Jurnal Ilmu Tanah dan Lingkungan (Journal of Soil Science and Environment) Mesin Limits: Journal of Mathematics and Its Applications International Journal of Aviation Science and Engineering
H Muhammad
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Aerospace Engineering Agriculture, Biological Sciences & Forestry Automotive Engineering Electrical & Electronics Engineering Environmental Science Mathematics Mechanical Engineering Transportation

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Journal : Mesin

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DEVELOPMENT OF COAXIAL ROTOR MICRO UNMANNED AERIAL VEHICLE Thien, H. P; Mulyanto, T; Muhammad, H; Suzuki, S
Mesin Vol 24, No 2 (2009)
Publisher : Mesin

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (861.224 KB)

Abstract

Micro Unmanned Helicopter with ability of takeoff, landing and hovering offeres excellent support tool for missions in indoor environment. In this paper, a review of preliminary studies towards the development of autonomous coaxial helicopter MAV is presented. The paper starts with the statement of coaxial helicoper MAV development. Then, it is continued by the introduction of development of dynamic model for a typical coaxial rotor platform. In the third issues, initial steps in development of sensory system and control system will be dealt with. In brief, an analytical mathematical model has successful derived. This model together with the developed sensor system will act important role towards the full development of the dynamics model as the system identification is carried out.
PEMBUATAN DAN PENGUJIAN SENSOR ULTRASONIK SEBAGAI FEEDBACK PADA SISTEM KENDALI OTOMATIK PITCH ATTITUDE HOLD Zaeny, U. M; Indriyanto, T; Muhammad, H
Mesin Vol 22, No 1 (2007)
Publisher : Mesin

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (445.206 KB)

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.
PEMBUATAN DAN PENGUJIAN SENSOR ULTRASONIK SEBAGAI FEEDBACK PADA SISTEM KENDALI OTOMATIK PITCH ATTITUDE HOLD U. M Zaeny; T Indriyanto; H Muhammad
Mesin Vol. 22 No. 1 (2007)
Publisher : Mesin

Show Abstract | Download Original | Original Source | Check in Google Scholar

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.
DEVELOPMENT OF COAXIAL ROTOR MICRO UNMANNED AERIAL VEHICLE H. P Thien; T Mulyanto; H Muhammad; S Suzuki
Mesin Vol. 24 No. 2 (2009)
Publisher : Mesin

Show Abstract | Download Original | Original Source | Check in Google Scholar

Abstract

Micro Unmanned Helicopter with ability of takeoff, landing and hovering offeres excellent support tool for missions in indoor environment. In this paper, a review of preliminary studies towards the development of autonomous coaxial helicopter MAV is presented. The paper starts with the statement of coaxial helicoper MAV development. Then, it is continued by the introduction of development of dynamic model for a typical coaxial rotor platform. In the third issues, initial steps in development of sensory system and control system will be dealt with. In brief, an analytical mathematical model has successful derived. This model together with the developed sensor system will act important role towards the full development of the dynamics model as the system identification is carried out.
Co-Authors A Rachim Ahmad Zaeny Canh, C X H Adijuwana H. P Thien I. Pranoto Indriyanto, T Mahayana, D Miswanto Mulyanto, T S Sabiham S Suzuki Suzuki, S T Indriyanto T Mulyanto Thien, H. P U. M Zaeny Zuhal, L R