Computational Questions of Equilibrium Calculation with Application to Nonlinear Aircraft Dynamics
1996 (English)In: Proceedings of the 1996 International Symposium on the Mathematical Theory of Networks and Systems, 1996Conference paper (Refereed)
The computation of possible stationary orientations of an aircraft subjected to constraints on actuators is treated using methods from computer algebra. The same techniques are also used to investigate possible turn maneuvers of a missile subjected to actuator constraints. The paper also gives a brief introduction to the utilized algebraic methods, cylindricalalgebraic decomposition and quantifier elimination.
Place, publisher, year, edition, pages
Nonlinear, Equilibrium, Aircraft
IdentifiersURN: urn:nbn:se:liu:diva-93743OAI: oai:DiVA.org:liu-93743DiVA: diva2:628144
1996 International Symposium on the Mathematical Theory of Networks and Systems, St. Louis, MO, USA, June, 1996
FunderSwedish Research Council