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Optimal linear quadratic powered descent with an intermediate point
Or Nataf,
Vitaly Shaferman
Aerospace Engineering
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Dive into the research topics of 'Optimal linear quadratic powered descent with an intermediate point'. Together they form a unique fingerprint.
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Keyphrases
Guidance Law
100%
Terminal Velocity
100%
Control Effort
100%
Linear Quadratic
100%
Powered Descent
100%
Analytical Solution
50%
Parametric Investigation
50%
Realistic Simulation
50%
Gravitational Field
50%
Performance Prediction
50%
Point Mass
50%
Miss Distance
50%
Optimal Control
50%
3D Point
50%
Quadratic Cost Function
50%
Velocity Error
50%
Mass Dynamics
50%
Propellant Consumption
50%
Soft Landing
50%
Ascent Guidance
50%
Ground Collisions
50%
Engineering
Powered Descent
100%
Terminal Velocity
100%
Closed Form Solution
50%
Good Performance
50%
Quadratic Cost
50%
Cost Function
50%
Performance Prediction
50%
Optimal Control
50%
Computer Science
Good Performance
100%
Gravitational Field
100%