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Tuesday, October 13, 2020 | History

1 edition of Computer simulated missile-target engagement with a Luenberger Observer and a ground observer found in the catalog.

Computer simulated missile-target engagement with a Luenberger Observer and a ground observer

Gerald L. Painter

Computer simulated missile-target engagement with a Luenberger Observer and a ground observer

by Gerald L. Painter

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Published by Naval Postgraduate School, Available from the National Technical Information Service in Monterey, Calif, Springfield, Va .
Written in English


About the Edition

The technique of proportional navigation is applied to a three dimensional missile-target engagement model. A Luenberger observer is developed to reduce the effects of noise or jamming to the missile"s seeker head. A ground observer which computes the deviations in target position and velocity and uplinks the deviations to the missile is also evaluated using the Kalman Filter theory to determine the benefits of the additional information provided to the missile.

Edition Notes

Statement Gerald L. Painter
The Physical Object
Pagination96 p. ;
Number of Pages96
ID Numbers
Open LibraryOL25504373M

o Successful demonstration of a simulated Ground-Based Interceptor engagement on a radar track from Sea-Based X-band Radar using a live target (March ) • Ground Tests o Successful assessment of ability of the Ballistic Missile Defense System to simultaneously execute multiple. N Challenges of distributed simulation execution, including data latency, data rates, and synchro-nization N Management and coordination of complex test requirements N Common threat and environment for stimulation of simulation elements N Methods for HWIL verification, validation, and accreditation. The ballistic missile defense system.

The latter allows to hit not only the ground infrastructure but also can be used as anti-ship weapons. “‘Iskander,’ like a good gun, allows the hunter to select the cartridge according to.   Technological and geopolitical factors have driven increased global supply and demand for high-velocity, unmanned, missile-based weapons and their corresponding counters. Besides more recognized cruise and ballistic missile threats, global missile proliferation now consists of a spectrum including precision-guided rockets, antiship missiles, air defenses, hypersonic delivery.

Figure displays the ground track view of the baseline engagement (same as Figure ) and compares it with the case of sec additional time delays between intercept and launch of each remaining interceptor in the four-shot SLS sequence. In short, if the second interceptor is launched in a normal SLS sequence and there is a failure. Guidance Control of a Missile With Noisy Inertial Sensors Modelling of the Inertial Sensors and Analysis of Error Sources. Comparison of the Linear Homing, Parabolic.


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Computer simulated missile-target engagement with a Luenberger Observer and a ground observer by Gerald L. Painter Download PDF EPUB FB2

Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection Computer simulated missile-target engagement with a Luenberger Observer and a ground observer. An illustration of a computer application window Wayback Machine.

An illustration of an open book. Books An illustration of two cells of a film strip. Computer simulated missile-target engagement with a Luenberger Observer and a ground observer Item Preview remove-circlePages: COMPUTER SIMULATED MISSILE-TARGET ENGAGEMENT WITH A LUENBERGER OBSERVER AND A GROUND OBSERVER by GERALD L.

PAINTER June, Thesis Advisor: H.A. Titus Approved for public release; distribution is unlimited. l i l t 1 0.

Computer simulated missile-target engagement with a Luenberger Observer and a ground observer. By Gerald L. Painter. Download PDF (5 MB) Abstract. Approved for public release; distribution is technique of proportional navigation is applied to a three dimensional missile-target engagement model.

Author: Gerald L. Painter. Computer Simulated Missile-Target Engagement With a Luenberger Observer and a Ground Observer missile-target engagement model. A Luenberger observer is developed to reduce the effects of noise. LFCTi8 THESIS COMPUTER SIMULATED MISSILE-TARGET ENGAGEMENT WITH A LUENBERGER OBSERVER AND A GROUND OBSERVER by GERALD L.

Access to Saline River in Benton (updated ) Lisa Spencer at Lisa's bait shop () said bass fishing is good in the river at this time.

Congratulations on deciding to install EmoTracker. Using the linearized missile target engagement model, an LQR based guidance law is designed to minimize the miss distance.

the nonlinear gain function in the observer. Simulation results show. Comput. & Elect. Engng, Vol. 1, pp. Periamon Press, Printed in Great Britain. DIGITAL COMPUTER TRAJECTORY SIMULATION OF AN AIR-TO-AIR MISSILE D.

KRUSKA and S. HOVANESSIAN Hughes Aircraft Company, Canoga Park, California, U.S.A. (Received 28 July ) Abstract-A procedure for solving and programming the Newtonian equations of motion for an air-to-air. provides the ability to create a more complex scene for MDS testing. The ICBM is a ground-launched three-stage target.

Modified Ballistic Re-Entry Vehicle and Countermeasures: TC develops cost-effective Modified Ballistic Re-Entry Vehicles in several different varieties and multiple configurations of countermeasure solutions with systematic rigor. Missile Simulation Matlab. In this paper an extended state observer (ESO) based guidance law is proposed for hit-to-kill interceptors in the three-dimensional high-speed engagement.

An. There are many approaches towards observer design, such as the Luenberger observer, the high gain observer, the H ∞ observer and the observer based on Kalman filter [11]. Sliding mode observers.

Engagement Scenario: This is a planar engagement, in which both the target and the missile are assumed t o be point mass models moving with constant speed. The target initiates an %g evasive maneuver a t the start of the engagement, switches to a dive maneuver of Sg after two seconds and continues with it till the end of the engagement.

A Simple Model for Calculating Ballistic Missile Defense Effectiveness satellite into orbit. 6 Moreover, ballistic missile proliferation may be accompa- nied by fewer tests and, hence, less accurate data compared to U.S.

and Rus. Guidance Control of a Missile With Noisy Inertial Sensors Modelling of the Inertial Sensors and Analysis of Error Sources. Design Of The Guidance And Control Missile.

dinated Engagement Simulation (ACES) to contrast the performance of the aforemen-tioned schemes in a realistic simulation environment. The distributions of raid outcomes for each scheme under two configurations,ideal and achievable, are compared. Operating conditions are examined through selecting real-world options and modeling underlying.

This thesis deals with a simulation of a missile versus target'engageent scenario. After deriving simplified transfer functions for the missile seeker head, missile autcmissile dynamics, and target dynamics, a three dimensional simulation is developed using classical proportional navigation.

The is simulated using state. Medium range ballistic missiles (MRBM) – capability. It is known that the total reaction of the missile at to km; any instant has two components, the lift and drag. For this reason, a comparative evaluation using simulation techniques was performed on a simple model, using both the OC and PN concepts.

The sample problem concerns a small homing missile in a low-altitude air-to-ground engagement, with the target assumed stationary. The pertinent geometry is depicted in Figure 5. Most publications discussing missile interception systems assume a zero computer response time.

This thesis studies the impact of computer response time on single-missile single-target and multiple- missile multiple-target systems. Simulation results for the final miss distance as the computer response time increases are presented. Whereas, the computer based non-destructiv e simulation can provide a cost-effective alternative to field trials.

An effort has been made to model the IR scene signature using virtual reality modelling tools and integrating this model into the missile-target engagement and countermeasure simulator.The intent of this book is to present the fundamental concepts of guided missiles, both tactical, and strategic and the guidance, control, and instrumenta-tion needed to acquire a target.

In essence, this book is about the mathematics of guided flight. This book differs from similar books on the subject in that it presents a. Washington, D.C., Decem - The SAC [Strategic Air Command] Atomic Weapons Requirements Study forproduced in June and published today for the first time by the National Security Archiveprovides the most comprehensive and detailed list of nuclear targets and target systems that has ever been far as can be told, no .