scispace - formally typeset
R

Robert F. Stengel

Researcher at Princeton University

Publications -  213
Citations -  8708

Robert F. Stengel is an academic researcher from Princeton University. The author has contributed to research in topics: Control system & Robustness (computer science). The author has an hindex of 40, co-authored 213 publications receiving 8369 citations. Previous affiliations of Robert F. Stengel include Massachusetts Institute of Technology & Charles Stark Draper Laboratory.

Papers
More filters
Journal ArticleDOI

Stochastic optimal therapy for enhanced immune response.

TL;DR: The inclusion of state estimation extends the applicability of optimal control theory for developing new therapeutic protocols to enhance immune response by addressing the effects that corrupted or incomplete measurements of the dynamic state may have on neighboring-optimal feedback control.
Journal ArticleDOI

Stochastic measures of performance robustness in aircraft control systems

TL;DR: 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 and confidence intervals for comparing two control system designs are presented.
Journal ArticleDOI

Manual attitude control of the lunar module

TL;DR: Manual attitude control for the Lunar Module employing directional stability, coordinated turn and attitude command is described in this paper, where the authors employ a turn-and-assistive attitude control.
Journal ArticleDOI

Stalling Characteristics of a General Aviation Aircraft

TL;DR: In this paper, the authors compared the stalling characteristics of a single-engine aircraft with flight test results using nonlinear simulation and linear stability and control evaluation, using aerodynamic and thrust characteristics obtained from a full-scale test in the NASA Langley Research Center 30 X 60ft Wind Tunnel as well as subscaie model test data.
Journal ArticleDOI

Effects of displacement and rate saturation on the control of statically unstable aircraft

TL;DR: In this paper, the effects of deflection and rate saturation on the stability of a statically unstable aircraft are investigated using the linear-quadratic (LQ) regulator, with the LQ regulator taken as the fundamental solution, and analytical and computational estimates of the stability limits imposed by control saturation are presented.