Abstract
Stochastic robustness, a simple technique used to estimate the robustness of linear, time-invariant systems, is applied to a twin-jet transport aircraft control system. Concepts behind stochastic stability robustness are extended to stochastic performance robustness. Stochastic performance robustness measures based on classical design specifications and measures specific to aircraft handling qualities are introduced. Confidence intervals for comparing two control system designs are presented. The application of stochastic performance robustness, the use of confidence intervals, and tradeoffs between performance objectives are demonstrated by means of the twin-jet aircraft example.
Original language | English (US) |
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Pages (from-to) | 1381-1387 |
Number of pages | 7 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 15 |
Issue number | 6 |
DOIs | |
State | Published - Nov 1992 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Applied Mathematics
- Electrical and Electronic Engineering
- Control and Systems Engineering
- Space and Planetary Science