John J. Deyst
Massachusetts Institute of Technology
48 Papers
615 Citations
John J. Deyst is an academic researcher from Massachusetts Institute of Technology. The author has contributed to research in topics: Redundancy (engineering) & Fault detection and isolation. The author has an hindex of 21, co-authored 48 publications. Previous affiliations of John J. Deyst include Charles Stark Draper Laboratory.
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Papers
A New Nonlinear Guidance Logic for Trajectory Tracking
Sanghyuk Park,John J. Deyst,Jonathan P. How +2 more
- 16 Aug 2004
TL;DR: In this paper, a nonlinear guidance logic for UAVs on curved trajectories is presented, which uses inertial speed in the computation of commanded lateral acceleration and adds adaptive capability to the change of vehicle speed due to external disturbances, such as wind.
Performance and Lyapunov Stability of a Nonlinear Path Following Guidance Method
TL;DR: In this paper, the adaptive nature of the guidance method makes its stability independent of vehicle velocity, and the stability analysis is also extended to show robust stability in the presence of saturated lateral acceleration, which is an inherent limitation of flight vehicles.
456
Existing and Required Modeling Capabilities for Evaluating ATM Systems and Concepts
Amedeo R. Odoni,Jeremy Bowman,Daniel Delahaye,John J. Deyst,Eric Feron,R. John Hansman,Kashif A. Khan,James K. Kuchar,Nicolas Pujet,Robert W. Simpson +9 more
- 01 Mar 1997
TL;DR: In this article, the authors assess the strengths and weaknesses of existing fast-time models and tools for the study of ATM systems and concepts and identify and prioritize the requirements for the development of additional modeling capabilities in the near future.
148
Patent
Integrated flight information and control system
R. John Hansman,Richard P. Kornfeld,John J. Deyst +2 more
- 08 Jul 1998
TL;DR: In this article, an improved navigation and display system especially suitable for small aircraft rapidly determines the attitude (roll and pitch) of an aircraft from measurements made by an inexpensive, single receiver and antenna responsive to signals obtained from a satellite positioning system.
68
Dual-Sensor Failure Identification Using Analytic Redundancy
TL;DR: In this article, the authors present a reliable technique for failure detection and identification for dual flight control sensors aboard the F-8 digital fly-by-wire aircraft, and discuss the successful application of the technique to identifying failures injected on test flight downlink data.
65