# overview
Dr. Vadali specializes on optimal control of space vehicles, orbital mechanics and aircraft flight dynamics and control.

# keywords[]
4009 Electronics, Sensors And Digital Hardware

# keywords[]
5102 Atomic, Molecular And Optical Physics

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4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# educationAndTraining[].organization.label
Virginia Tech - (Blacksburg, Virginia, United States)

# publications[].label
DESIGN OF SATELLITE FORMATIONS IN ORBITS OF HIGH ECCENTRICITY WITH PERFORMANCE CONSTRAINTS SPECIFIED OVER A REGION OF INTEREST

# publications[].label
Design of Satellite Formations in Orbits of High Eccentricity with Performance Constraints Specified over a Region of Interest

# publications[].label
The characterization of formation flying satellite relative motion orbits

# publications[].label
NEURAL-NETWORK-BASED CONTROL OF LARGE STRUCTURES

# publications[].publisher
SPIE, the international society for optics and photonics

# publications[].label
Suboptimal command generation for control moment gyroscopes and feedback control of spacecraft

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
SPACE STATION ATTITUDE-CONTROL AND MOMENTUM MANAGEMENT - A NONLINEAR LOOK

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Space Station attitude control and momentum management - A nonlinearlook

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Optimal variable-structure control tracking of spacecraft maneuvers

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
FEEDBACK CONTROL OF FLEXIBLE SPACECRAFT LARGE-ANGLE MANEUVERS USING LIAPUNOV THEORY.

# publications[].label
Spacecraft Formation Flying: Dynamics, Control, and Navigation

# publications[].label
Optimal Solar Sail Trajectory Analysis for Interstellar Missions

# publications[].label
LINEAR STATE-SPACE MODELS FOR J2-PERTURBED SATELLITE RELATIVE MOTION

# publications[].label
FEEDFORWARD FEEDBACK-CONTROL LAW FOR NEAR TIME-OPTIMAL SPACECRAFT REORIENTATION

# publications[].label
COMPARISON OF ORBIT ELEMENT SETS FOR MODELING PERTURBED SATELLITE RELATIVE MOTION

# publications[].label
OPTIMAL SOLAR SAIL TRAJECTORY ANALYSIS FOR INTERSTELLAR MISSIONS

# publications[].label
FEEDBACK-CONTROL AND STEERING LAWS FOR SPACECRAFT USING SINGLE GIMBAL CONTROL MOMENT GYROS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ANALYTIC SOLUTION OF PERTURBED RELATIVE MOTION WITH ZONAL AND TESSERAL HARMONICS

# publications[].label
A series solution method for the solution of the Hamilton Jacobi Isaacs equation and its applications to aerospace systems

# publications[].label
FEEDBACK-CONTROL AND STEERING LAWS FOR SPACECRAFT USING SINGLE GIMBAL CONTROL MOMENT GYROS

# publications[].label
Analytical solution for power-limited optimal rendezvous near an elliptic orbit

# publications[].label
Orbit determination of a tethered satellite system using laser and radar tracking

# publications[].label
A novel control design methodology for maintaining position and attitude of a power-sail

# publications[].label
Input shaped control of 3-dimensional maneuvers of flexible spacecraft

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
SUBOPTIMAL COMMAND GENERATION FOR CONTROL MOMENT GYROSCOPES AND FEEDBACK-CONTROL OF SPACECRAFT

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Linear and Nonlinear Control Laws for Formation Flying

# publications[].label
A Magnus Series-Based Modified Sweep Method for Optimal Control

# publications[].label
NEAR-MINIMUM TIME OPEN-LOOP SLEWING OF FLEXIBLE VEHICLES

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ROBUST-CONTROL OF LINEAR-SYSTEMS WITH UNCERTAIN PARAMETERS USING TIME-DELAYED INPUTS

# publications[].label
A new concept for controlling formation flying satellite constellations

# publications[].label
Initial conditions and fuel-optimal control for formation flying of satellites

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ANALYTIC SOLUTION FOR SATELLITE RELATIVE MOTION WITH ZONAL GRAVITY PERTURBATIONS

# publications[].label
Formation Maintenance and Fuel Balancing for Satellites with Implusive Control

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Modeling and control of satellite formations in high eccentricity orbits

# publications[].label
THIRD-BODY PERTURBATION EFFECTS ON SATELLITE FORMATIONS

# publications[].label
Gyroless attitude control of multibody satellites using an unscented Kalman filter

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
QUASI CLOSED-FORM SOLUTION TO THE TIME-OPTIMAL RIGID SPACECRAFT REORIENTATION PROBLEM

# publications[].label
Optimal design of satellite formation relative motion orbits using least squares methods

# publications[].label
Verification of Optimality and Costate Estimation Using Hilbert Space Projection

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Semianalytic Computation of Ballistic Transfers in the Restricted Three-Body Problem

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Spacecraft formation flying control using mean orbit elements

# publications[].label
Modelling and Simulation of a Power Sail

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Optimal Nonlinear Feedback Control Design Using a Waypoint Method

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
QUASI-CLOSED-FORM SOLUTION TO THE TIME-OPTIMAL RIGID SPACECRAFT REORIENTATION PROBLEM

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Periodic relative motion near a Keplerian elliptic orbit with nonlinear differential gravity

# publications[].label
Sub-optimal formation establishment and reconfiguration using impulsive control

# publications[].label
The successive backward sweep method for optimal control of nonlinear systems with constraints

# publications[].label
Optimal Formation Design for Magnetospheric Multiscale Mission Using Differential Orbital Elements

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Near-minimum-time maneuvers of large structures - Theory and experiments

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Local Manifolds and Periodic Orbits Around Equilibrium Points of the Rotating Mass Dipole

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ROBUST CONTROL OF SPACECRAFT ROTATIONAL MANEUVERS.

# publications[].label
Satellite formation design in orbits of high eccentricity with performance constraints specified over a region of interest: MMS phase II

# publications[].label
Autonomous Rendezvous Architecture Design for Lunar Lander

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
NEAR-MINIMUM-TIME MANEUVERS OF LARGE STRUCTURES - THEORY AND EXPERIMENTS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Development of a state transition matrix for relative motion using the unit sphere approach

# publications[].label
Special Issue John L. Junkins Dynamical Systems Symposium Celebrating 50 Orbits of Academic Excellence Texas A&M University College Station, TX May 20-21, 2018

# publications[].label
BRIDGING DYNAMICAL MODELING EFFORT AND SENSOR ACCURACY IN RELATIVE SPACECRAFT NAVIGATION

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Optimal finite-time feedback controllers for nonlinear systems with terminal constraints

# publications[].label
A simplified formulation of the satellite perturbed relative motion problem

# publications[].label
FEEDBACK TETHER DEVELOPMENT AND RETRIEVAL

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Modeling and control of satellite formations in high eccentricity orbits

# publications[].label
Satellite orbit transfer and formation reconfiguration via an attitude control analogy

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Spaceflight Mechanics 2006 - Proceedings of the AAS/AIAA Space Flight Mechnaics Meeting: Preface

# publications[].label
International space station leak localization using vent torque estimation

# publications[].label
Relative motion and the geometry of formations in Keplerian elliptic orbits

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ROBUST TIME-DELAY CONTROL OF MULTIMODE SYSTEMS

# publications[].publisher
Institute of Electrical and Electronics Engineers (IEEE)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
TWO-BODY ORBITAL BOUNDARY VALUE PROBLEMS IN REGULARIZED COORDINATES

# publications[].label
Large-Angle Kinematics for the Control of Satellite Relative Motion

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ANALYTIC SOLUTION FOR SATELLITE RELATIVE MOTION: THE COMPLETE ZONAL GRAVITATIONAL PROBLEM

# publications[].label
Linear and nonlinear control laws for formation flying

# publications[].label
Formation design and geometry for Keplerian elliptic orbits with arbitrary eccentricity

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Touch points in optimal ascent trajectories with first-order state inequality constraints

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
TIME-OPTIMAL TRAJECTORY DESIGN FOR A DUAL-SATELLITE SAILCRAFT INTERSTELLAR MISSION WITH PROBE RELEASE

# publications[].label
OPTIMAL OPEN-LOOP AND STABLE FEEDBACK-CONTROL OF RIGID SPACECRAFT ATTITUDE MANEUVERS

# publications[].label
Advances in the Astronautical Sciences: Preface

# publications[].label
Computation of near-minimum-time maneuvers of flexible structures byparameter optimization

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ADAPTIVE-CONTROL AND MOMENTUM MANAGEMENT OF SPACECRAFT WITH UNKNOWN-PARAMETERS AND DISTURBANCES

# publications[].label
Third-Body Perturbation Effects on Satellite Formations

# publications[].label
Satellite Orbit Design and Maintenance for Terrestrial Coverage

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
NEAR-OPTIMAL 3-DIMENSIONAL ROTATIONAL MANEUVERS OF SPACECRAFT USING MANIPULATOR ARMS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Averaged relative motion and applications to formation flight near perturbed orbits

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Formation Flying Satellites: Control by an Astrodynamicist

# publications[].label
Optimal finite-time feedback controllers for nonlinear systems with terminal constraints

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Optimal rotational maneuvers of spacecraft using manipulator arms

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Spacecraft Formation Flying: Dynamics, control and navigation Introduction

# publications[].label
An intelligent control concept for formation flying satellites

# publications[].label
State-Transition Matrix for Satellite Relative Motion in the Presence of Gravitational Perturbations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
THREE-DIMENSIONAL TIME OPTIMAL MULTI-REVERSAL ORBIT BY USING HIGH PERFORMANCE SOLAR SAILS

# publications[].label
Higher Order Methods for Determining Optimal Controls and Their Sensitivities

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ROBUST TIME-OPTIMAL CONTROL - FREQUENCY-DOMAIN APPROACH

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Special issue: The John L. Junkins Astrodynamics Symposium - Preface

# publications[].label
Optimal Formation Design for the Magnetospheric Multiscale Mission Using Differential Orbital Elements

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Modeling issues related to retrieval of flexible tethered satellite systems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Formation establishment and reconfiguration using impulsive control

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Autonomous Lunar Orbit Rendezvous Guidance Based on J(2)-Perturbed State Transition Matrix

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Feedback control law for variable speed control moment gyros

# publications[].label
PREFERRED GIMBAL ANGLES FOR SINGLE GIMBAL CONTROL MOMENT GYROS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
USE OF THE WORK-ENERGY RATE PRINCIPLE FOR DESIGNING FEEDBACK-CONTROL LAWS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
NEW RESULTS ON THE OPTIMAL SPACECRAFT ATTITUDE MANEUVER PROBLEM

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Journal of the Astronautical Sciences: Preface

# publications[].label
NEAR-MINIMUM TIME, CLOSED-LOOP SLEWING OF FLEXIBLE SPACECRAFT

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
COMPUTATION OF NEAR-MINIMUM-TIME MANEUVERS OF FLEXIBLE STRUCTURES BY PARAMETER OPTIMIZATION

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Gyroless Attitude Control of Multi-Body Satellites Using an Unscented Kalman Filter

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Feedback control design for smooth, near minimum time rotational maneuvers of flexible spacecraft

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
OPTIMAL OPEN-LOOP AND FEEDBACK-CONTROL USING SINGLE GIMBAL CONTROL MOMENT GYROSCOPES

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Model for Linearized Satellite Relative Motion About a J(2)-Perturbed Mean Circular Orbit

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ATTITUDE-CONTROL AND MOMENTUM MANAGEMENT OF THE SPACE STATION

# publications[].label
Touch points in optimal ascent trajectories with first-order state inequality constraints

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Modeling and control of interferometric formations in the vicinity of the collinear libration points

# publications[].label
FEEDBACK CONTROL OF SPACECRAFT LARGE-ANGLE MANEUVERS USING REACTION WHEELS AND ON-OFF THRUSTERS.

# publications[].label
Periodic relative motion near a Keplerian elliptic orbit with nonlinear differential gravity

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Formation flying satellites: Control by an astrodynamicist

# publications[].label
Near minimum-time maneuvers of large space structures using parameter optimization

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An inverse-free technique for attitude control of spacecraft using CMGS

# publications[].label
Feedback control law for variable speed control moment gyros

# publications[].label
Analysis and Distributed Control of a Formation of Intelligent Satellites

# publications[].label
Robust time-delay control of multimode systems

# publications[].label
Parameter optimization using adaptive bound genetic algorithms

# publications[].label
Near-optimal feedback rendezvous in elliptic orbits accounting for nonlinear differential gravity

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Three-dimensional time Optimal Multi-reversal Orbit by Using Solar Sailing

# publications[].label
Spacecraft formation flying control using mean orbit elements

# publications[].label
A Lyapunov-based controller for satellite formation reconfiguration in the presence of J(2) perturbations

# publications[].label
Exact Delaunay normalization of the perturbed Keplerian Hamiltonian with tesseral harmonics

# publications[].label
Design of Satellite Formations in Orbits of High Eccentricity withPerformance Constraints Specified over a Region of Interest

# publications[].label
State Transition Matrix for relative motion including J2 and third-body perturbations

# publications[].label
Second-order state transition for relative motion near perturbed, elliptic orbits

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
PREFERRED GIMBAL ANGLES FOR SINGLE GIMBAL CONTROL MOMENT GYROS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Robust time-optimal control - A frequency domain approach

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ANALYSIS OF RELATIVE GPS NAVIGATION TECHNIQUES

# publications[].label
A hybrid trajectory optimization technique for the mars sample return mission

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Parameter identification for the International Space Station using nonlinear momentum management control

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
TRAJECTORY OPTIMIZATION USING PARALLEL SHOOTING METHOD ON PARALLEL COMPUTER

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
International Space Station Leak Localization Using Attitude Disturbance Estimation

# publications[].publisher
Institute of Electrical and Electronics Engineers (IEEE)

# publications[].label
Orbit establishment for formation flying of satellites

# publications[].label
OPTIMAL OPEN LOOP AND STABLE FEEDBACK CONTROL OF RIGID SPACECRAFT ATTITUDE MANEUVERS.

# publications[].label
NONLINEAR FEEDBACK DEPLOYMENT AND RETRIEVAL OF TETHERED SATELLITE SYSTEMS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A Recursive Formulation of the Satellite Perturbed Relative Motion Problem

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
RELATIVE MOTION STATE TRANSITION MATRIX INCLUDING GRAVITATIONAL PERTURBATIONS

# publications[].label
Higher Order Sensitivities for Solving Nonlinear Two-Point Boundary-Value Problems

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Optimal nonlinear feedback controller design using a waypoint scheme

# publications[].label
EXACT NORMALIZATION OF THE TESSERAL HARMONICS

# publications[].label
MODELING ISSUES RELATED TO RETRIEVAL OF FLEXIBLE TETHERED SATELLITE SYSTEMS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Examination of the optimal nonlinear regulator problem

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Spacecraft Momentum Management and Attitude Control Using a Receding Horizon Approach

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
OPTIMAL OPEN-LOOP AND FEEDBACK-CONTROL USING SINGLE GIMBAL CONTROL MOMENT GYROSCOPES

# publications[].label
ATTITUDE-CONTROL OF SPACECRAFT USING NEURAL NETWORKS

# publications[].label
On the fundamental frequencies of satellite relative motion and control of formations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Active control of structural-acoustic systems - Noise reduction in payload fairings

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
International space station leak localization using attitude response data

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Solution of optimal control/guidance problems using the parallel shooting method on a parallel computer

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
ISS leak localization using attitude response

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Optimal Design of Satellite Formation Relative Motion Orbits Using Least-Squares Methods

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Optimal strategies in cooperative games with terminal payoff

# publications[].label
Hill's equations, mean orbital elements, and formation flying of satellites

# publications[].label
STATE TRANSITION MATRIX FOR RELATIVE MOTION INCLUDING HIGHER-ORDER GRAVITY PERTURBATIONS

# publications[].label
Solar Sail Planar Multireversal Periodic Orbits

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Modeling and control of satellite formations in high eccentricity orbits

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Fundamental frequencies of satellite relative motion and control of formations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Design and control of libration point satellite formations

# publications[].label
FEEDBACK-CONTROL OF TETHERED SATELLITES USING LYAPUNOV STABILITY THEORY

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
The Basics of Analytical Mechanics, Optimization, Control and Estimation

# publications[].label
SIMULTANEOUS COMPUTATION OF OPTIMAL CONTROLS AND THEIR SENSITIVITIES

# publications[].label
Two-Body Orbital Boundary Value Problems in Regularized Coordinates

# publications[].label
Analysis and Distributed Control of a Formation of Intelligent Satellites

# publications[].label
Feedback control of tethered satellites using Liapunov stability theory

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An inverse-free technique for attitude control of spacecraft using CMGs

# publications[].label
INPUT-SHAPED CONTROL OF 3-DIMENSIONAL MANEUVERS OF FLEXIBLE SPACECRAFT

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Nonlinear Considerations In Satellite Formation Flying

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# researcherOn[].label
Relative Motion Modeling and Autonomous Navigation Accuracy

# researcherOn[].awardedBy.label
United States Air Force - (Arlington, Virginia, United States)

# streetAddress
Texas A&M University; Aerospace Engineering; 3141 TAMU