State-Transition Matrix for Satellite Relative Motion in the Presence of Gravitational Perturbations von Mahajan, Bharat, Vadali, Srinivas R, Alfriend, Kyle T

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Two-Body Orbital Boundary Value Problems in Regularized Coordinates von Mahajan, Bharat, Vadali, Srinivas R.

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Model for linearized satellite relative motion about a J(2)-perturbed mean circular orbit von Vadali Srinivas, R

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Autonomous Lunar Orbit Rendezvous Guidance Based on J2-Perturbed State Transition Matrix von Li, Jingyang, Vadali, Srinivas R., Baoyin, Hexi

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Formation Flying: Accommodating Nonlinearity and Eccentricity Perturbations von Vaddi, Sesha S, Vadali, Srinivas R, Alfriend, Kyle T

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Satellite Orbit Design and Maintenance for Terrestrial Coverage von Sengupta, Prasenjit, Vadali, Srinivas R, Alfriend, Kyle T

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Autonomous Rendezvous Architecture Design for Lunar Lander von Li, Jingyang, Baoyin, Hexi, Vadali, Srinivas R

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Optimal Nonlinear Feedback Control Design Using a Waypoint Method von Sharma, Rajnish, Vadali, Srinivas R, Hurtado, John E

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Model for Linearized Satellite Relative Motion About a J2-Perturbed Mean Circular Orbit von Vadali, Srinivas R

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Fundamental Frequencies of Satellite Relative Motion and Control of Formations von Vadali, Srinivas R, Sengupta, Prasenjit, Yan, Hui, Alfriend, Kyle T

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Second-order state transition for relative motion near perturbed, elliptic orbits von Sengupta, Prasenjit, Vadali, Srinivas R., Alfriend, Kyle T.

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Third-Body Perturbation Effects on Satellite Formations von T. Roscoe, Christopher W., Vadali, Srinivas R., Alfriend, Kyle T.

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A Magnus Series-Based Modified Sweep Method for Optimal Control von Cho, D. H., Vadali, Srinivas R.

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Relative Motion and the Geometry of Formations in Keplerian Elliptic Orbits with Arbitrary Eccentricity von Sengupta, Prasenjit, Vadali, Srinivas R

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Design of Satellite Formations in Orbits of High Eccentricity with Performance Constraints Specified over a Region of Interest von Roscoe, Christopher W T, Vadali, Srinivas R, Alfriend, Kyle T

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Spacecraft Formation Flying Control Using Mean Orbit Elements von Schaub, Hanspeter, Vadali, Srinivas R., Junkins, John L., Alfriend, Kyle T.

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Feedback Control Law for Variable Speed Control Moment Gyros von Schaub, Hanspeter, Vadali, Srinivas R, Junkins, John L

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Autonomous Lunar Orbit Rendezvous Guidance Based on J 2 -Perturbed State Transition Matrix von Li, Jingyang, Vadali, Srinivas R, Baoyin, Hexi

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International Space Station Leak Localization Using Attitude Response Data von Kim, Jong-Woo, Crassidis, John L, Vadali, Srinivas R, Dershowitz, Adam

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Nonlinear Finite-Horizon Regulation and Tracking for Systems with Incomplete State Information Using Differential State Dependent Riccati Equation von Khamis, Ahmed, Kamel, Ahmed M., Naidu, D. Subbaram

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