Ballistic entry motion, including gravity - Constant drag coefficient case

Author:

Hough Michael E.1

Affiliation:

1. The Analytic Sciences Corporation, Reading, Massachusetts

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference16 articles.

1. Alien, J. and Eggers, A. "A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth's Atmosphere at High Supersonic Speeds," NACA Report 1381, 1958.

2. Closed-Form Solution for Ballistic Vehicle Motion

3. A Second-Order Theory of Entry Mechanics Into a Planetary Atmosphere

4. An analytic solution for entry into planetary atmospheres

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1. Observability of a Thrusting/Ballistic Trajectory in 3-D From a Single Fixed Passive Sensor;IEEE Transactions on Aerospace and Electronic Systems;2018-12

2. Trajectory estimation and impact point prediction of a ballistic object from a single fixed passive sensor;Signal Processing, Sensor/Information Fusion, and Target Recognition XXVII;2018-04-27

3. Explicit guidance along an optimal space curve;Journal of Guidance, Control, and Dynamics;1989-07

4. Semi-analytic solution of a two-body problem with drag;Celestial Mechanics;1984-04

5. Ballistic entry motion using a generic inviscid drag model;Astrodynamics Conference;1982-08-09

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