E
Ernest Ohlmeyer
Researcher at Naval Surface Warfare Center
Publications - 46
Citations - 1653
Ernest Ohlmeyer is an academic researcher from Naval Surface Warfare Center. The author has contributed to research in topics: Missile & Missile guidance. The author has an hindex of 20, co-authored 46 publications receiving 1551 citations.
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Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads
TL;DR: In this paper, the authors developed a high fidelity, nine degree-of-freedom simulation model of a kinetic warhead with three moving-mass actuators, which is used for actuator sizing and in the development of flight control systems.
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Integrated Guidance and Control of Missiles With $theta hbox - D$ Method
TL;DR: In this paper, a new suboptimal control method is proposed to effectively design an integrated guidance and control system for missiles, which allows designers to bring together concerns about guidance law performance and autopilot responses under one unified framework.
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Integrated Design of Agile Missile Guidance and Autopilot Systems
TL;DR: In this paper, a technique for integrated design of missile guidance and autopilot systems using the feedback linearization technique is discussed, and numerical results using a six degree-of-freedom (FDF) missile simulation are given.
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Generalized Vector Explicit Guidance
Ernest Ohlmeyer,Craig Phillips +1 more
TL;DR: In this paper, the authors proposed a new guidance law termed generalized vector explicit guidance (GENEX), which can simultaneously achieve design specifications on miss distance and final missile-target relative orientation.
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Numerical State-Dependent Riccati Equation Approach for Missile Integrated Guidance Control
TL;DR: In this paper, the Riccati equation is used to describe the relative position components of the target with respect to a moving mass along the pitch and yaw axes of the body yc, zc = moving-mass position commands.