An Online Optimal Explicit Guidance Scheme for Long Range Missiles With Solid Motors

The International Conference on Electrical Engineering
doi 10.21608/iceeng.2010.33469
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Egypts Presidential Specialized Council for Education and Scientific Research

Related search

An Approximate Optimal Maximum Range Guidance Scheme for Subsonic Unpowered Gliding Vehicles

International Journal of Aerospace Engineering
Aerospace Engineering
2015English

Three-Dimensional Optimal Impact Time Guidance for Antiship Missiles

Journal of Guidance, Control, and Dynamics
ControlSystems EngineeringElectronic EngineeringApplied MathematicsSpaceElectricalPlanetary ScienceAerospace Engineering
2019English

Optimal Fixed-Interval Integrated Guidance-Control Laws for Hit-To-Kill Missiles

2003English

A New Optimal Guidance Law for Air-To-Air Missiles Against Evasive Targets.

Transactions of the Japan Society for Aeronautical and Space Sciences
SpacePlanetary ScienceAerospace Engineering
2000English

Optimal Controllers for Homing Missiles With Two Time Constants

1969English

An Optimal Acceptance Policy for an Urn Scheme

SIAM Journal on Discrete Mathematics
Mathematics
1998English

An Explicit Finite-Difference Scheme for Simulation of Moving Particles

English

Squeezing Lubrication Films: Layering Transition for Curved Solid Surfaces With Long-Range Elasticity

Journal of Chemical Physics
MedicineTheoretical ChemistryAstronomyPhysicsPhysical
2000English

An Optimal Key Management Scheme for Group Key Sharing With Polynomial Expression

Research Journal of Information Technology
Computer Science
2013English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy