How Nonlinear Is It? A Tutorial on Nonlinearity of Orbit and Attitude Dynamics

John L. Junkins, Puneet Singla

Research output: Contribution to journalConference articlepeer-review

1 Scopus citations


Some observations are made on coordinate selection for the two most fundamental problems of astrodynamics, namely orbit dynamics and attitude dynamics, and some interesting connections and analogies between the two problems are explored. While an infinity of coordinate choices are feasible for each of these problems, we review four coordinate choices for each problem, including several that lead to governing differential equations that are regular, and in some cases, rigorously linear. Some methodology is introduced that has a universal flavor with implications for dynamical systems broadly. We show how dramatic qualitative and quantitative alteration of the mathematical description of the motion can be accomplished by introduction of redundant coordinates to describe the evolution of the dynamics in a higher dimensioned space. Some observations are made on an analogy between the two central problems of astrodynamics: Spacecraft attitude dynamics and orbit dynamics. One of the regularizing transformations studied for orbital dynamics is motivated directly by this analogy. Finally broadly applicable analytical and computational developments are presented that provide a measure of nonlinearity over a worst-case region of state space in the vicinity of a reference trajectory; this measure is used to evaluate the several coordinate choices.

Original languageEnglish (US)
Pages (from-to)3-52
Number of pages50
JournalAdvances in the Astronautical Sciences
StatePublished - Dec 1 2003
EventThe John L. Junkins Astrodynamics Symposium: Proceedings of the Texas A and M Univeristy/AAS John L. Junkins Astrodynamics Symposium - College Station, TX, United States
Duration: May 23 2003May 24 2003

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science


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