Autonomous ascent guidance with multiple terminal constraints for all-solid launch vehicles

Applied Optimal Control

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Control Application, Mathematical Control Theory, Applied Optimal Control +1

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Flight Dynamics, Engineering, Aerospace Engineering +13

Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast Arcs

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Mathematical Programming, Numerical Analysis, Orbit Determination +14

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Motion Control, Engineering, Aerial Robotics +8

Particle swarm optimization applied to impulsive orbital transfers

Mauro Pontani, Bruce A. Conway · Acta Astronautica · 2012 · 82 citations

Aerospace Engineering, Firefly Algorithm, Hybrid Optimization Technique +2