Abstract
A control law is formulated to determine the motion of the simulator cab so that its motion will '%'best'%' approximate the desired aircraft response, and not exceed the limited translational capability of the simulator. Due to lack of experimental data, '%'best'%' can only be interpreted subjectively at the present time. By use of the method, a variety of quasi-optimal responses, each emphasizing different features thought to be important in motion perception, have been obtained. Examples of such results are given, and the considerations important in initial subjective evaluations by experienced flight personnel are discussed.
| Original language | English (US) |
|---|---|
| Journal | NASA Contractor Reports |
| State | Published - 1970 |
| Externally published | Yes |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering