1984 · 16 citations · 2 references
Natural SciencesAerospace EngineeringMathematicsDifferential EquationsDynamical SystemsFlight DynamicsControl Of Dynamical SystemsControl TheoryNonlinear ControlNumerical ConvergenceNumerical Methods For Differential EquationsSystems Of Differential EquationsBackward Difference SchemesConvergenceDifferential Equation SolversFinite Difference ApproximationFinite Difference SchemesNonlinear Differential-algebraic EquationsNumerical ModelingSpace Shuttle Reentry
The equations which describe a trajectory prescribed path control (TPPC) problem naturally form a system of nonlinear semi-explicit, differential-algebraic equations (DAES) with index greater than one. It is known that not all implicit systems may be solved stably by the k-step backward difference formulas (BDF), yet these methods do produce convergent numerical solutions to some semi-explicit systems. Convergence theory of the BDF for DAE systems are briefly reviewed, before discussing our numerical experience with the simplest BDF when applied to an index three, TPPC problem that arose in the reentry control of the Space Shuttle.
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