Abstract
Similarity transformations which preserve modal characteristics and acceleration cues in aircraft in-flight simulation are presented. A velocity-mismatch example illustrates that acceleration matching is achieved at the expense of mismatching in cues which are secondary to the simulated piloting task, while primary cues are preserved. The approach is applicable for both implicit and explicit model following, and it can be easily extended to the longitudinal case.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 538-540 |
| Number of pages | 3 |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 2 |
| Issue number | 6 |
| State | Published - Nov 1979 |
All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
- Aerospace Engineering
- Space and Planetary Science
- Electrical and Electronic Engineering
- Applied Mathematics