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@lamont-granquist
Created July 14, 2023 19:59
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https://arc.aiaa.org/doi/10.2514/1.G005493 - Orbital Guidance Using Higher-Order State Transition Tensors

https://arc.aiaa.org/doi/10.2514/1.G004434 - Trajectory Design via Convex Optimization for Six-Degree-of-Freedom Asteroid Powered Landing

https://arc.aiaa.org/doi/10.2514/1.G005340 - Autonomous Navigation of Relativistic Spacecraft in Interstellar Space

https://arc.aiaa.org/doi/10.2514/1.G005376 - Convex Approach to Three-Dimensional Launch Vehicle Ascent Trajectory Optimization

https://arc.aiaa.org/doi/10.2514/1.G005503 - Three-Dimensional Path-Following Control for an Underwater Vehicle

https://arc.aiaa.org/doi/10.2514/1.G005839 - Rapid Low-Thrust Trajectory Optimization in Deep Space Based on Convex Programming

https://arc.aiaa.org/doi/10.2514/1.G005395 - Low-Thrust Maneuverability Using Bilinear Tangent Guidance near Small Bodies

https://arc.aiaa.org/doi/10.2514/1.G004812 - Onboard Real-Time Generation of Launch Vehicle Abort Orbits

https://arc.aiaa.org/doi/10.2514/1.G005978 - Bearings-Only Guidance in Cis-Lunar Rendezvous

https://arc.aiaa.org/doi/10.2514/1.G005918 - Optimal Bi-Impulse Orbital Transfers: Station Keeping Applications

https://arc.aiaa.org/doi/10.2514/1.G005890 - Variable Time-of-Flight Spacecraft Maneuver Targeting Using State Transition Tensors

https://arc.aiaa.org/doi/10.2514/1.G005224 - Analytic Costate Initialization from Rough State-Trajectory Estimates

https://arc.aiaa.org/doi/10.2514/1.G005827 - Analytical Estimation of the Velocity Increment in J2-Perturbed Impulsive Transfers

https://arc.aiaa.org/doi/10.2514/1.G006361 - Point Mascon Global Lunar Gravity Models

https://arc.aiaa.org/doi/10.2514/1.G006091 - Fast Solver for J2-Perturbed Lambert Problem Using Deep Neural Network

https://arc.aiaa.org/doi/10.2514/1.G006373 - Direct Solution of the Keplerian State Transition Matrix

https://arc.aiaa.org/doi/10.2514/1.G006430 - Circular Restricted n-Body Problem

https://arc.aiaa.org/doi/10.2514/1.G006502 - Analytical Costate Estimation by a Reference Trajectory-Based Least-Squares Method

https://arc.aiaa.org/doi/10.2514/1.G006741 - Three-Dimensional Guidance Law Mimicking Realistic Ballistic Trajectories

https://arc.aiaa.org/doi/10.2514/1.G006558 - Higher-Order Lambert Problem Solution Based on Differential Algebra

https://arc.aiaa.org/doi/10.2514/1.G006644 - Analytical State Propagation for Continuous-Thrust Linear Relative Motion

https://arc.aiaa.org/doi/10.2514/1.G006970 - Revised Picard–Chebyshev Methods for Perturbed Orbit Propagations

https://arc.aiaa.org/doi/10.2514/1.G006671 - Picard Iteration-Based Convexification for Fuel-Optimal Rocket Descent Inside Atmosphere

https://arc.aiaa.org/doi/10.2514/1.G006899 - Finite-Horizon Near-Optimal Approach and Landing Planning of Reusable Launch Vehicles

https://arc.aiaa.org/doi/10.2514/1.G006766 - Sequential Convex Programming Using Augmented Lagrange Multiplier Method and Concave–Convex Decomposition

https://arc.aiaa.org/doi/10.2514/1.G007091 - Exploiting Scaling Constants to Facilitate the Convergence of Indirect Trajectory Optimization Methods

https://arc.aiaa.org/doi/10.2514/1.G006977 - Smoothing Homotopy Methods for Solving Nonlinear Optimal Control Problems

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