Nonlinear Recursive Filter for Boost Trajectories

A nonlinear recursive algorithm is formulated for state vector and covariance estimation of boost trajectories. The thrust acceleration vector of the booster is modeled by a vector-differential equation that includes effects of propellant depletion and attitude motions resulting from gravity-turn ma...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2001-09, Vol.24 (5), p.991-997
1. Verfasser:	Hough, Michael E
Format:	Artikel
Sprache:	eng
Schlagworte:	Accuracy Algorithms Applied sciences Boosters (rocket) Computer science control theory systems Control theory. Systems Differential equations Dynamics Exact sciences and technology IIR filters Kalman filtering Mathematical models Modelling and identification Monte Carlo methods Monte Carlo simulation Nonlinear control systems State estimation Vector quantization Velocity
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