Relative Maneuver and Minimum Effort Guidance Under Gravity
Author:
Affiliation:
1. Chinese Academy of Ordnance Sciences,Beijing,China,100089
2. Beijing Institute of Astronautical Systems Engineering,Beijing,China,100076
3. School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China,100081
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10239690/10239711/10240271.pdf?arnumber=10240271
Reference13 articles.
1. Gravity-Turn-Assisted Optimal Guidance Law
2. Optimal Rocket Landing Guidance Using Convex Optimization and Model Predictive Control
3. Three-Dimensional Impact Angle Guidance Laws Based on Model Predictive Control and Sliding Mode Disturbance Observer
4. State-Dependent Riccati-Equation-Based Guidance Law for Impact-Angle-Constrained Trajectories
5. Applied Optimal Control
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