DOCSLIB.ORG
Explore
Sign Up
Log In
Upload
Search
Home
» Tags
» Osculating orbit
Osculating orbit
Low Thrust Manoeuvres to Perform Large Changes of RAAN Or Inclination in LEO
Osculating Orbit Elements and the Perturbed Kepler Problem
Astrodynamics
Orbit Options for an Orion-Class Spacecraft Mission to a Near-Earth Object
Orbit Determination Using Modern Filters/Smoothers and Continuous Thrust Modeling
Orbit Conjunction Filters Final
Satellite Orbits
Statistical Orbit Determination
New Closed-Form Solutions for Optimal Impulsive Control of Spacecraft Relative Motion
Lecture Notes on Space Mechanics
Non-Averaged Regularized Formulations As an Alternative to Semi-Analytical Orbit Propagation Methods
A Delta-V Map of the Known Main Belt Asteroids
Analytical Low-Thrust Trajectory Design Using the Simplified General Perturbations Model J
In-Orbit Lifetime Prediction for Leo and Heo Based on Orbit Determination from Tle Data
Arxiv:2004.00037V2 [Astro-Ph.EP] 26 May 2020
Symplectic Map Description of Halley's Comet Dynamics
New Method and Analysis of Proximity Trajectory-Only Learned Dynamics for Small Body Gravity Fields
Determination of Mean Atmospheric Densities from the Explorer Ix Satellite
Top View
ISTS-2017-D-023ⅠISSFD-2017-023
Orbital Mechanics Third Edition
Relative Orbital Motion Dynamical Models for Orbits About Nonspherical Bodies
Reference Systems in Satellite Geodesy
MONITORING and MITIGATION of CLOSE PROXIMITIES in LOW EARTH ORBIT S. Aida(1)
Of Satemite Mition to a Lunar Orbiter
C 2018 by Bindu Bhargavi Jagannatha. All Rights Reserved. SPACE LOGISTICS NETWORK OPTIMIZATION with EMBEDDED PROPULSION TECHNOLOGY SELECTION
Spacecraft Formation Flying Control Using Mean Orbit Elements
1 Chapter 13 Calculation of Orbital Elements 13.1
A Satellite Footprint Visualisation Tool
The Full Two-Body-Problem: Simulation, Analysis, and Application to the Dynamics, Characteristics, and Evolution of Binary Asteroid Systems
Direct Evaluation of the Earth's Gravity Anomaly Field from Orbital Analysis of Artificial Earth Satellites
Note on the Dynamical Evolution of C/2017 K2 PANSTARRS
Program Cover Design and Printing Costs Sponsored by Analytical Graphics
Near-Earth Objects in Earthlike Orbits
Symplectic Map Description of Halley's Comet Dynamics
3 Newtonian Orbital Dynamics
Investigating Analytical and Numerical Methods to Predict Satellite Orbits Using Two-Line Element Sets Adam T
Accuracy Assessment of Sgp4 Orbit Information Conversion Into Osculating Elements
Introduction This Memo Was Undertaken to Update Someof the Information That Has Grown Stale in the Mars Observer Planetary Constants and Models Document (Ref 1)
Dynamical Evolution of C/2017 K2 PANSTARRS Małgorzata Królikowska1 and Piotr A
Lecture Notes of SPACE MECHANICS Based on the Notes for the SPACECRAFT ORBITAL DYNAMICS and CONTROL Course of the University of Bologna Written by Dr
Development of an Interplanetary Orbital Propagator
Preprint) AAS 19-909
Compact Binary Inspiral: Nature Is Perfectly Happy with a Circle
Real-Time Estimation of Sgp4 Orbital Elements from Gps Navigation Data
The Flyby Anomaly: a Multivariate Analysis Approach
Non-Averaged Regularized Formulations As an Alternative to Semi-Analytical Orbit Propagation Methods
Calculation of Ephemerides from Initial Values
Dynamics and Distribution of Jovian Dust Ejected from the Galilean Satellites
An Analytical Theory for the Perturbative Effect of Solar
AAS/AIAA Astrodynamics Specialist Conference
Spacecraft Relative Orbit Description Through Orbit Element Differences
Asymptotic Solution for the Orbit Motion Under Constant Tangential Acceleration1
The Orbital Pericenter Precession in the 2PN Approximation
Approaches for Modeling Satellite Relative Motion
A Survey and Performance Analysis of Orbit Propagators for LEO, GEO, and Highly Elliptical Orbits
Development of Space Surveillance Tracking and Orbit Determination Program
User's Manual