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Effects of aircraft design on stol ride quality: a simulator study
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jacobson, I. D. Jones, C. R. |
| Copyright Year | 1974 |
| Description | To improve the ride quality in short takeoff aircraft, several means have been investigated. In general, these methods consist of placing sensors in the aircraft which sense aircraft motion, usually linear accelerations and angular rates. These signals are then used to deflect control surfaces which generate aerodynamic forces and moments which tend to minimize the motion which the passenger feels. One of the disadvantages of some of these systems is that they may tend to degrade the handling qualities or controllability of the airplane, making it more difficult or annoying for the pilot to fly. Rather than using active control systems to control ride quality, one might possibly design aircraft so that they are inherently pleasant to ride. The purpose of this study is to determine the relationship between characteristic aircraft motions and aircraft ride quality. |
| File Size | 512707 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740024330 |
| Archival Resource Key | ark:/13960/t78s9h56w |
| Language | English |
| Publisher Date | 1974-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Flight Characteristics Aircraft Stability Data Acquisition Comfort Human Reactions Aircraft Performance Human Factors Engineering Short Takeoff Aircraft Flight Control Flight Simulation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
