Amanote Research

Amanote Research

    RegisterSign In

Optimal Two-Impulse Trajectories With Moderate Flight Time for Earth-Moon Missions

Mathematical Problems in Engineering - Egypt
doi 10.1155/2012/971983
Full Text
Open PDF
Abstract

Available in full text

Categories
MathematicsEngineering
Date

January 1, 2012

Authors
Sandro da Silva FernandesCleverson Maranhão Porto Marinho
Publisher

Hindawi Limited


Related search

JSS Multispectral Imagers for Earth Observation Missions

English

Optimal Controllers for Homing Missiles With Two Time Constants

1969English

Minimum Impulse Three-Body Trajectories

1973English

Optimal Trajectories for Homing Navigation With Bearing Measurements

IFAC Proceedings Volumes
2008English

A Hierarchical Flight Planner for Sensor-Driven UAV Missions

2013English

Optical Communications Systems for NASA's Human Space Flight Missions

2019English

Direct Earth/Moon Cargo Delivery

2005English

Evolution of the Earth – Moon System

Planetary Science
2014English

Real-Time Optimal Mission Scheduling and Flight Path Selection

IEEE Transactions on Automatic Control
ControlSystems EngineeringComputer Science ApplicationsElectricalElectronic Engineering
2007English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy