Abstract
A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.
| Original language | English |
|---|---|
| Title of host publication | International Workshop on Advanced Motion Control, AMC |
| Pages | 62-65 |
| Number of pages | 4 |
| Volume | 2006 |
| DOIs | |
| Publication status | Published - 2006 |
| Externally published | Yes |
| Event | 9th IEEE International Workshop on Advanced Motion Control, 2006 - Istanbul Duration: 2006 Mar 27 → 2006 Mar 29 |
Other
| Other | 9th IEEE International Workshop on Advanced Motion Control, 2006 |
|---|---|
| City | Istanbul |
| Period | 06/3/27 → 06/3/29 |
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ASJC Scopus subject areas
- Engineering(all)
Cite this
Takeoff and landing control using force sensor by electrically-powered helicopters. / Shimada, Akira; Fujita, Masanori.
International Workshop on Advanced Motion Control, AMC. Vol. 2006 2006. p. 62-65 1631633.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Takeoff and landing control using force sensor by electrically-powered helicopters
AU - Shimada, Akira
AU - Fujita, Masanori
PY - 2006
Y1 - 2006
N2 - A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.
AB - A takeoff and landing control of helicopters using a force sensor helicopter is introduced. The system consists of a small electrically-powered helicopter, a flight base under which the focre sensor is set, and a helicopter control terminal which is connected to a system controller. When the helicopter stands on the base, the force sensor outputs data corresponding to the weight of the helicopter. As the operational voltage rises, the helicopter almost take off from the base. Concurrently, the forse sensor output closes to 0. It means that lift force related to force output becomes from 0 N to the value cprresponding to the weight. This paper introduces the design process including system modeling and the experimental results.
UR - http://www.scopus.com/inward/record.url?scp=33751034888&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=33751034888&partnerID=8YFLogxK
U2 - 10.1109/AMC.2006.1631633
DO - 10.1109/AMC.2006.1631633
M3 - Conference contribution
AN - SCOPUS:33751034888
VL - 2006
SP - 62
EP - 65
BT - International Workshop on Advanced Motion Control, AMC
ER -