Guidance and control of a launch vehicle using a stochastic gradient projection method

DOI10.1016/S0005-1098(99)00163-6zbMath0968.93526WikidataQ126590531 ScholiaQ126590531MaRDI QIDQ1975578

Fernando Madeira, Atair Rios Neto

Publication date: 13 September 2001

Published in: Automatica (Search for Journal in Brave)

Mathematics Subject Classification ID

Application models in control theory (93C95)

Uses Software

• OTIS

Cites Work

• Unnamed Item
• Parallel solver for trajectory optimization search directions
• Geometric synthesis of aerospace plane ascent guidance logic
• Stochastic processes and filtering theory
• An explicit closed-loop guidance for launch vehicles
• Rapid near-optimal aerospace plane trajectory generation and guidance
• Optimal control of ascent trajectories and rotary dynamics for wingless orbital stages
• Direct trajectory optimization using nonlinear programming and collocation
• Discrete approximations to optimal trajectories using direct transcription and nonlinear programming
• Finite element method for optimal guidance of an advanced launch vehicle
• Trajectory optimization based on differential inclusion (Revised)
• Trajectory optimization on a parallel processor
• The Optimization of Trajectories
• Use of polynomial approximations to calculate suboptimal controls

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