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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.

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Optimal transition from entry to cruising flight

TL;DR: Optimal angle of attack transition trajectories for space shuttle from atmospheric entry to cruising flight for conventional airport landing as mentioned in this paper, for a single flight of the Space Shuttle from the International Space Station to an airport landing.

Modern digital flight control system design for VTOL aircraft

TL;DR: In this article, a digital flight control system (DFCS) for a CH-47B helicopter is presented, which employed proportional integral control logic to provide rapid, precise response to automatic or manual guidance commands while following conventional or spiral-descent approach paths.
Journal ArticleDOI

From the Earth to the Moon: A Freshman Seminar

TL;DR: From the Earth to the Moon as discussed by the authors is a course for first-year undergraduate students that deals with both technical and non-technical aspects of space flight, with particular reference to lunar voyages.
Proceedings ArticleDOI

Nonlinear Inverse Dynamics Control Laws - A Sampled Data Approach

TL;DR: In this paper, a sampled data approach for the implementation of nonlinear inverse dynamics (NID) control laws in real time is presented, where the control laws place the same number of poles as their continuous-time counterparts, take into account the system dynamics in between the sample points, and embed the computational delays associated with the inverse calculations directly into their design.

Quantitative knowledge acquisition for expert systems

TL;DR: In this article, a statistical method is presented for generating rule bases from numerical data, motivated by an example based on aircraft navigation with multiple sensors, and the specific objective is to design an expert system that selects a satisfactory suite of measurements from a dissimilar, redundant set, given an arbitrary navigation geometry and possible sensor failures.