Control, and Dynamics Journal of Guidance - Texas A&M University (TAMU) Scholar

publication venue for

Distributed Absolute and Relative Estimation of Spacecraft Formations. 46:1126-1141. 2023
Linear Quadratic Regulator Weighting Matrices for Output Covariance Assignment in Nonlinear Systems. 46:264-276. 2023
Orthogonal Approximation of Invariant Manifolds in the Circular Restricted Three-Body Problem. 1-12. 2023
Factorized Partial-Update Schmidt-Kalman Filter. 45:1567-1582. 2022
Nonlinear Gaussian Mixture Filtering with Intrinsic Fault Resistance. 44:2172-2185. 2021
Eclipse-Conscious Transfer to Lunar Gateway Using Ephemeris-Driven Terminal Coast Arcs. 44:1972-1988. 2021
Optimal Bi-Impulse Orbital Transfers: Station Keeping Applications. 44:2057-2066. 2021
Low-Thrust Gravity-Assist Trajectory Design Using Optimal Multimode Propulsion Models. 44:1280-1294. 2021
Least Sum of Absolute Residuals Orbit Determination. 45:468-480. 2021
Computationally Efficient Attitude Estimation with Extended H-2 Filtering. 44:418-427. 2021
Impartial Sensor Tasking via Forecasted Information Content Quantification. 43:2031-2045. 2020
Anonymous Feature-Based Terrain Relative Navigation. 43:410-421. 2020
Multiple-Timescale Nonlinear Control of Aircraft with Model Uncertainties. 43:536-552. 2020
State-Transition Matrix for Satellite Relative Motion in the Presence of Gravitational Perturbations. 42:1441-1457. 2019
Optimal-Transport-Based Tracking of Space Objects Using Range Data from a Single Ranging Station. 42:1237-1249. 2019
Nonlinear Differential Equation Solvers via Adaptive Picard-Chebyshev Iteration: Applications in Astrodynamics. 42:1007-1022. 2019
Second-Order Integral-Form Gauss's Variational Equations Under Impulsive Control. 42:284-302. 2019
Exploration of Alternative State Vector Choices for Low-Thrust Trajectory Optimization. 42:47-64. 2019
Nielsen, Tzenoff, and Other Equation Forms for Variable-Mass Systems. 42:149-152. 2019
Hamilton's Principle for Variable-Mass Systems. 41:2647-+. 2018
Generic Smoothing for Optimal Bang-Off-Bang Spacecraft Maneuvers. 41:2470-2475. 2018
Trajectory-Driven Adaptive Control of Autonomous Unmanned Aerial Vehicles with Disturbance Accommodation. 41:1-14. 2018
Analytical Dynamics of Variable-Mass Systems. 41:701-709. 2018
Considering Uncertain Parameters in Non-Gaussian Estimation for Single-Target and Multitarget Tracking. 40:2138-2150. 2017
Fault-Tolerant Adaptive Model Inversion Control for Vision-Based Autonomous Air Refueling. 40:1336-1347. 2017
Design of Constellations for Earth Observation with Intersatellite Links. 40:1261-1269. 2017
Sparse Approximation-Based Collocation Scheme for Nonlinear Optimal Feedback Control Design. 40:248-264. 2017
Synthesis and Flight Test of Automatic Landing Controller Using Quantitative Feedback Theory. 39:1994-2010. 2016
Solar Sail Body-Fixed Hovering over Elongated Asteroids. 39:1223-1231. 2016
Optimal Transport Approach for Probabilistic Robustness Analysis of F-16 Controllers. 38:1935-1946. 2015
Bearings-Only Initial Relative Orbit Determination. 38:1699-1713. 2015
Multiple-Object Space Surveillance Tracking Using Finite-Set Statistics. 38:1741-1756. 2015
Optical Short-Arc Association Hypothesis Gating via Angle-Rate Information. 38:1602-1613. 2015
Projecting High-Dimensional Parametric Uncertainties for Improved State Estimation Error Confidence. 38:1659-1672. 2015
Uncertain Lambert Problem. 38:1573-1584. 2015
Sensitivity Methods Applied to Orbital Pursuit Evasion. 38:1118-U217. 2015
Autonomous Lunar Orbit Rendezvous Guidance Based on J(2)-Perturbed State Transition Matrix. 38:315-321. 2015
Collision Probability with Gaussian Mixture Orbit Uncertainty. 37:979-984. 2014
Photometric Attitude Estimation for Agile Space Objects with Shape Uncertainty. 37:921-932. 2014
Solar Sail Planar Multireversal Periodic Orbits. 37:674-681. 2014
Attitude Error Kinematics. 37:330-U24. 2014
Joseph Formulation of Unscented and Quadrature Filters with Application to Consider States. 36:1871-1874. 2013
Probabilistic Initial Orbit Determination Using Gaussian Mixture Models. 36:1324-1335. 2013
Entropy-Based Approach for Uncertainty Propagation of Nonlinear Dynamical Systems. 36:1047-1057. 2013
Guaranteed Approach for Orbit Determination with Limited Error Measurements. 36:1186-1193. 2013
Removing Space Debris Through Sequential Captures and Ejections. 36:743-752. 2013
Analysis of the Monotonic Lagrangian Grid as an Air Traffic Simulation Tool. 36:196-206. 2013
Small Unmanned Aircraft: Theory and Practice. 36:344-345. 2013
Kalman Filter for Linear Fractional Order Systems. 35:1816-1827. 2012
Review of Steady Aircraft Flight and Performance by N. Harris McClamroch. 35:1023-1024. 2012
Analytical Nonlinear Propagation of Uncertainty in the Two-Body Problem. 35:497-509. 2012
Optimization of Perimeter Patrol Operations Using Unmanned Aerial Vehicles. 35:434-441. 2012
Sampling-Based Path Planning for a Visual Reconnaissance Unmanned Air Vehicle. 35:619-631. 2012
Analytical Study of Tangent Orbit and Conditions for Its Solution Existence. 35:186-194. 2012
Nonlinear Filter Based on the Fokker-Planck Equation. 35:68-79. 2012
Time-Varying Deadbeat Controller Design. 35:284-295. 2012
Kinetic State Tracking for a Class of Singularly Perturbed Systems. 34:734-749. 2011
Optimal Nonlinear Feedback Control Design Using a Waypoint Method. 34:698-705. 2011
Rock-Around Orbits. 34:810-819. 2011
Dispersion Analysis in Hypersonic Flight During Planetary Entry Using Stochastic Liouville Equation. 34:459-474. 2011
Hypersonic State Estimation Using the Frobenius-Perron Operator. 34:325-344. 2011
Nonlinear Estimation of Hypersonic State Trajectories in Bayesian Framework with Polynomial Chaos. 33:1765-1778. 2010
Observer/Kalman-Filter Time-Varying System Identification. 33:887-900. 2010
Constrained Multiple-Revolution Lambert's Problem. 33:1779-1786. 2010
Linear-Parameter-Varying Control of an Improved Three-Degree-of-Freedom Aeroelastic Model. 33:615-619. 2010
Cayley Family of Attitude Coordinates. 33:246-249. 2010
Model for Linearized Satellite Relative Motion About a J(2)-Perturbed Mean Circular Orbit. 32:1687-1691. 2009
Multibody Model of an Ornithopter. 32:1675-1679. 2009
Norm-Constrained Kalman Filtering. 32:1458-1465. 2009
Solution of Two-Point Boundary-Value Problems Using Lagrange Implicit Function Theorem. 32:1684-1687. 2009
New Results for Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft. 32:1071-1076. 2009
Verification of Optimality and Costate Estimation Using Hilbert Space Projection. 32:1345-1355. 2009
Optimal Design of Satellite Formation Relative Motion Orbits Using Least-Squares Methods. 32:599-604. 2009
Computational Nonlinear Stochastic Control. 32:1050-1055. 2009
Inertial Measurements from Flight Data of a Flapping-Wing Ornithopter. 32:326-331. 2009
Interior Parameters, Exterior Parameters, and a Cayley-Like Transform. 32:653-657. 2009
Distributed Formation Flight Control Using Constraint Forces. 32:112-120. 2009
Fundamental frequencies of satellite relative motion and control of formations. 31:1239-1248. 2008
Structured adaptive model inversion controller for Mars atmospheric flight. 31:937-953. 2008
Prediction of icing effects on the coupled dynamic response of light airplanes. 31:656-673. 2008
Averaged relative motion and applications to formation flight near perturbed orbits. 31:258-272. 2008
Reentry time prediction using atmospheric density corrections. 31:282-289. 2008
Decentralized cooperative-control design for multivehicle formations. 31:970-979. 2008
Fuel-efficient interferometric imaging maneuvers in near-Earth orbit. 31:1133-1144. 2008
Lagrangian view of the work-rate theorem. 31:1508-1511. 2008
Gyroless attitude control of multibody satellites using an unscented Kalman filter. 31:245-251. 2008
Boom and receptacle autonomous air refueling using visual snake optical sensor. 30:1753-1769. 2007
Near-optimal feedback rendezvous in elliptic orbits accounting for nonlinear differential gravity. 30:1803-1813. 2007
Review of Flight Dynamics. 30:1836-1838. 2007
Determining Strictly Positive Realness from System Modal Characteristics. 30:1539-1542. 2007
Digital autoland control laws using quantitative feedback theory and direct digital design. 30:1399-1413. 2007
Motion planning under uncertainty: Application to an unmanned helicopter. 30:1268-1276. 2007
Approximate minimum energy control laws for low-thrust formation reconfiguration. 30:1182-1185. 2007
Pseudospectral feedback control for three-axis magnetic attitude stabilization in elliptic orbits. 30:1107-1115. 2007
Relative motion and the geometry of formations in Keplerian elliptic orbits. 30:953-964. 2007
Prediction of icing effects on the dynamic response of light airplanes. 30:722-732. 2007
Angles-only orbit updates for low-Earth-orbit satellites. 30:314-321. 2007
Differential Semimajor Axis Estimation Performance Using Carrier-Phase Differential Global Positioning System Measurements. 30:301-313. 2007
Fuel optimal maneuvers for multispacecraft interferometric imaging systems. 30:227-236. 2007
Optimal linear attitude estimator. 30:1619-1627. 2007
Aircraft landing scheduling optimization for single runway noncontrolled airports: Static case. 30:252-255. 2007
Kalman filtering for relative spacecraft attitude and position estimation. 30:133-143. 2007
Linear feedback control using quasi velocities. 29:1309-1314. 2006
Solving Linear and Quadratic Quaternion Equations. 29:1420-1423. 2006
International space station leak localization using attitude response data. 29:1041-1050. 2006
Periodic relative motion near a Keplerian elliptic orbit with nonlinear differential gravity. 29:1110-1121. 2006
Adaptive output feedback control for spacecraft rendezvous and docking under measurement uncertainty. 29:892-902. 2006
Optimal finite-time feedback controllers for nonlinear systems with terminal constraints. 29:921-928. 2006
Trajectory tracking controller for vision-based probe and drogue autonomous aerial refueling. 29:846-857. 2006
Fault-tolerant structured adaptive model inversion control. 29:635-642. 2006
Dynamic shape control of a morphing airfoil using spatially distributed transducers. 29:612-616. 2006
Orbit design for ground surveillance using genetic algorithms. 29:1231-1235. 2006
Optimal Servicing of Geosynchronous Satellites. 29:203-206. 2006
Satellite orbit transfer and formation reconfiguration via an attitude control analogy. 28:1200-1209. 2005
Path Planning and Open-Loop Shape Control of Modular Tensegrity Structures. 28:421-430. 2005
Suppression of control reversal using leading- and trailing-edge control surfaces. 28:452-460. 2005
Evaluation and comparison of relative motion theories. 28:254-261. 2005
Formation establishment and reconfiguration using impulsive control. 28:262-268. 2005
Convergence of Newton's method via Lyapunov analysis. 28:363-365. 2005
Precision Tracking Control Against Dynamic Targets for High-Energy Laser Systems. 28:30-35. 2005
Vision-based sensor and navigation system for autonomous air refueling. 28:979-989. 2005
Anytime control algorithm: Model reduction approach. 27:767-776. 2004
Control of a nonlinear wing section using leading- and trailing-edge surfaces. 27:52-58. 2004
State transition matrix of relative motion for the perturbed noncircular reference orbit. 26:956-971. 2003
Evaluation of longitudinal desired dynamics for dynamic-inversion controlled generic reentry vehicles. 26:811-819. 2003
Precise ephemeris reconstruction using the Clohessy-Wiltshire frame and multiple sequential compressions. 26:781-785. 2003
Structured model reference adaptive control for a class of nonlinear systems. 26:551-557. 2003
Formation flying: Accommodating nonlinearity and eccentricity perturbations. 26:214-223. 2003
Observer/Kalman filter identification for online system identification of aircraft. 26:347-353. 2003
Comparison of agility metrics to Beck agility metrics using linear error theory. 26:19-26. 2003
Nonlinear receding horizon control of an F-16 aircraft. 25:924-931. 2002
Fuel-optimal, low-thrust, three-dimensional Earth-Mars trajectories. 24:1100-1107. 2001
Fuel-optimal, low-thrust, three-dimensional Earth-Mars trajectories. 24:1100-1107. 2001
Impulsive feedback control to establish specific mean orbit elements of spacecraft formations. 24:739-745. 2001
Agility metric robustness using linear]Error theory. 24:340-351. 2001
Multiresolution Methods for Reduced-Order Models for Dynamical Systems. 24:193-200. 2001
Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics. 24:95-100. 2001
Nonlinear Control Methods for High-Energy Limit-Cycle Oscillations. 24:185-192. 2001
Identification and control of limit cycle oscillations in aeroelastic systems. 23:1127-1133. 2000
Probability of collision between space objects. 23:769-772. 2000
Adaptive hysteresis model for model reference control with actuator hysteresis. 23:459-465. 2000
Fuel-optimal planar Earth-Mars trajectories using low-thrust exhaust-modulated propulsion. 23:476-482. 2000
Optimal variable-structure control tracking of spacecraft maneuvers. 23:564-566. 2000
Second estimator of the optimal quaternion. 23:885-888. 2000
Singularity avoidance using null motion and variable-speed control moment gyros. 23:11-16. 2000
Do All Linear Flexible Structures Have Convergent Second-Order Observers?. 22:905-908. 1999
Eigenstructure assignment algorithm for mechanical second-order systems. 22:729-731. 1999
Autonomous Maneuver Tracking for Self-Piloted Vehicles. 22:624-624. 1999
Controller Design of Periodic Time-Varying Systems via Time-Invariant Methods. 22:486-488. 1999
Autonomous maneuver tracking for self-piloted vehicles. 22:58-67. 1999
Autonomous maneuver tracking for self-piloted vehicles (vol 22, pg 58, 1999). 22:624-624. 1999
Applied active control for a nonlinear aeroelastic structure. 21:838-845. 1998
Stability and control of a structurally nonlinear aeroelastic system. 21:718-725. 1998
Touch points in optimal ascent trajectories with first-order state inequality constraints. 21:603-610. 1998
Euler-q algorithm for attitude determination from vector observations. 21:328-334. 1998
Optimal near-minimum-time control. 21:172-174. 1998
Editorial: Nonlinear dynamical systems. 20:1057-1057. 1997
Nonlinear adaptive control of spacecraft maneuvers. 20:1104-1110. 1997
Nonlinear control of a prototypical wing section with torsional nonlinearity. 20:1181-1189. 1997
Orthogonal square root eigenfactor parameterization of mass matrices. 20:1118-1124. 1997
Higher-order Cayley transforms with applications to attitude representations. 20:528-534. 1997
New penalty functions and optimal control formulation for spacecraft attitude control problems. 20:428-434. 1997
N-dimensional cross product and its application to matrix eigenanalysis. 20:509-515. 1997
Adventures on the interface of dynamics and control. 20:1058-1071. 1997
Lyapunov optimal saturated control for nonlinear systems. 20:1083-1088. 1997
Dynamics and stability of a freely precessing spacecraft containing a nutation damper. 19:297-304. 1996
NEAR-MINIMUM-TIME MANEUVERS OF LARGE STRUCTURES - THEORY AND EXPERIMENTS. 18:1380-1385. 1995
SUBOPTIMAL COMMAND GENERATION FOR CONTROL MOMENT GYROSCOPES AND FEEDBACK-CONTROL OF SPACECRAFT. 18:1350-1354. 1995
MODELING ISSUES RELATED TO RETRIEVAL OF FLEXIBLE TETHERED SATELLITE SYSTEMS. 18:1169-1176. 1995
EIGENVECTOR DERIVATIVES FOR MECHANICAL 2ND-ORDER SYSTEMS. 18:899-906. 1995
Low-Earth-orbit maintenance - Reboost vs thrust-drag cancellation. 18:930-932. 1995
NEAR-OPTIMAL 3-DIMENSIONAL ROTATIONAL MANEUVERS OF SPACECRAFT USING MANIPULATOR ARMS. 18:932-934. 1995
Covariance control design for Hubble Space Telescope. 18:230-236. 1995
TRAJECTORY OPTIMIZATION USING PARALLEL SHOOTING METHOD ON PARALLEL COMPUTER. 18:377-379. 1995
Reduced-Order Model Based Control of the Flexible, Articulated-Truss Space Crane. 18:135-142. 1995
VALIDATION OF FINITE-DIMENSIONAL APPROXIMATE SOLUTIONS FOR DYNAMICS OF DISTRIBUTED-PARAMETER SYSTEMS. 18:87-95. 1995
Integrated modeling and control for the Large Spacecraft Control Laboratory experiment facility. 17:442-450. 1994
COMPUTATION OF NEAR-MINIMUM-TIME MANEUVERS OF FLEXIBLE STRUCTURES BY PARAMETER OPTIMIZATION. 17:354-360. 1994
Modeling Hubble Space Telescope flight data by Q-Markov cover identification. 17:250-256. 1994
ROBUST TIME-OPTIMAL CONTROL - FREQUENCY-DOMAIN APPROACH. 17:346-353. 1994
INPUT-SHAPED CONTROL OF 3-DIMENSIONAL MANEUVERS OF FLEXIBLE SPACECRAFT. 16:1061-1068. 1993
INVARIANT SET ANALYSIS OF THE HUB-APPENDAGE PROBLEM. 16:1191-1193. 1993
ACTIVE CONTROL TECHNOLOGY FOR LARGE SPACE STRUCTURES. 16:801-821. 1993
MANEUVER AND VIBRATION CONTROL OF HYBRID COORDINATE SYSTEMS USING LYAPUNOV STABILITY THEORY. 16:668-676. 1993
QUASI-CLOSED-FORM SOLUTION TO THE TIME-OPTIMAL RIGID SPACECRAFT REORIENTATION PROBLEM. 16:453-461. 1993
Q-Markov covariance equivalent realization and its application to flexible structure identification. 16:308-319. 1993
EXPLICIT GENERALIZATION OF LAGRANGE EQUATIONS FOR HYBRID COORDINATE DYNAMIC-SYSTEMS (J GUIDANCE, VOL 15, PG 1443, 1992). 16:224-224. 1993
EXPLICIT GENERALIZATION OF LAGRANGE EQUATIONS FOR HYBRID COORDINATE DYNAMIC-SYSTEMS. 15:1443-1452. 1992
Structure redesign for improved dynamic response. 15:1272-1278. 1992
SPACE STATION ATTITUDE-CONTROL AND MOMENTUM MANAGEMENT - A NONLINEAR LOOK. 15:577-586. 1992
NEAR-MINIMUM-TIME CONTROL OF A FLEXIBLE MANIPULATOR. 15:477-481. 1992
NONLINEAR FEEDBACK DEPLOYMENT AND RETRIEVAL OF TETHERED SATELLITE SYSTEMS. 15:28-34. 1992
USE OF THE WORK-ENERGY RATE PRINCIPLE FOR DESIGNING FEEDBACK-CONTROL LAWS. 15:275-277. 1992
MEASURE OF CONTROLLABILITY FOR ACTUATOR PLACEMENT. 14:895-902. 1991
FEEDBACK-CONTROL OF TETHERED SATELLITES USING LYAPUNOV STABILITY THEORY. 14:729-735. 1991
LOW-AUTHORITY EIGENVALUE PLACEMENT FOR 2ND-ORDER STRUCTURAL SYSTEMS. 14:698-701. 1991
FEEDBACK TETHER DEVELOPMENT AND RETRIEVAL. 14:469-470. 1991
NEAR-MINIMUM-TIME CONTROL OF DISTRIBUTED PARAMETER-SYSTEMS - ANALYTICAL AND EXPERIMENTAL RESULTS. 14:406-415. 1991
PREFERRED GIMBAL ANGLES FOR SINGLE GIMBAL CONTROL MOMENT GYROS. 13:1090-1095. 1990
Sensitivity controller for uncertain systems. 13:321-329. 1990
NONLINEAR FLIGHT CONTROL DESIGN VIA SLIDING METHODS. 13:850-858. 1990
NEAR-MINIMUM TIME, CLOSED-LOOP SLEWING OF FLEXIBLE SPACECRAFT. 13:57-65. 1990
ROBUST EIGENSTRUCTURE ASSIGNMENT BY A PROJECTION METHOD - APPLICATIONS USING MULTIPLE OPTIMIZATION CRITERIA. 12:396-403. 1989
ROBUST EIGENSYSTEM ASSIGNMENT FOR FLEXIBLE STRUCTURES. 12:381-387. 1989
NEAR-MINIMUM TIME OPEN-LOOP SLEWING OF FLEXIBLE VEHICLES. 12:82-88. 1989
ROBUSTNESS OPTIMIZATION OF STRUCTURAL AND CONTROLLER PARAMETERS. 12:89-96. 1989
IDENTIFICATION METHOD FOR LIGHTLY DAMPED STRUCTURES. 11:571-576. 1988
Erratum. 11:0480b-0480b. 1988
FINITE-TIME MATRIX CONVOLUTION INTEGRAL SENSITIVITY CALCULATIONS. 11:473-475. 1988
MINIMUM MODEL ERROR ESTIMATION FOR POORLY MODELED DYNAMIC-SYSTEMS. 11:256-261. 1988
RE-EXAMINATION OF EIGENVECTOR DERIVATIVES. 10:581-587. 1987
A SEQUENTIAL LINEAR OPTIMIZATION APPROACH FOR CONTROLLER-DESIGN. 9:699-703. 1986
AN ASYMPTOTIC PERTURBATION METHOD FOR NONLINEAR OPTIMAL-CONTROL PROBLEMS. 9:391-396. 1986
VARIABLE-STRUCTURE CONTROL OF SPACECRAFT LARGE-ANGLE MANEUVERS. 9:235-239. 1986
OPTIMAL NONLINEAR FEEDBACK-CONTROL FOR SPACECRAFT ATTITUDE MANEUVERS. 9:99-107. 1986
EIGENVALUE OPTIMIZATION ALGORITHMS FOR STRUCTURE CONTROLLER-DESIGN ITERATIONS. 8:697-706. 1985
Dynamics and control of lattice beams using simplified finite element models. 8:612-619. 1985
Identification of vibrating flexible structures. 8:463-470. 1985
SPACE STRUCTURE CONTROL DESIGN BY VARIANCE ASSIGNMENT.. 8:54-62. 1985
Space structure control design by variance assignment. 8:454-462. 1985
DISTRIBUTED PIEZOELECTRIC POLYMER ACTIVE VIBRATION CONTROL OF A CANTILEVER BEAM. 8:605-611. 1985
ROBUST NONLINEAR LEAST-SQUARES ESTIMATION USING THE CHOW-YORKE HOMOTOPY METHOD. 7:752-755. 1984
An analytic orbit prediction program generator. 7:575-581. 1984
Minimal root sensitivity in linear systems. 7:570-574. 1984
NEW RESULTS ON THE OPTIMAL SPACECRAFT ATTITUDE MANEUVER PROBLEM. 7:378-380. 1984
IDENTIFICATION OF LARGE FLEXIBLE STRUCTURES MASS STIFFNESS AND DAMPING FROM ON-ORBIT EXPERIMENTS. 7:244-245. 1984
Model Reference Adaptive Control of Large Structural Systems. 6:112-118. 1983
Discrete-Time Stability of Continuous-Time Controller Designs for Large Space Structures. 5:541-543. 1982
Order reduction for models of space structures using modal cost analysis. 5:351-357. 1982
COMMENT ON OPTIMAL FEEDBACK SLEWING OF FLEXIBLE SPACECRAFT. 5:318-318. 1982
Controllability and Observability for Flexible Spacecraft. 3:452-459. 1980
Optimal Continuous Torque Attitude Maneuvers. 3:210-217. 1980
Local Representation of the Geopotential by Weighted Orthonormal Polynomials. 3:55-61. 1980
Orthogonal Filters for Model Error Compensation in the Control of Nonrigid Spacecraft. 1:41-49. 1978
Simultaneous design of active vibration control and passive viscous damping. 1:90-93. 1978
QuateRA: The Quaternion Regression Algorithm 2020
Derived Angle of Attack and Sideslip Angle Characterization for General Aviation 2020
Bezier Description of Space Trajectories 2016
Synthesis and Flight Test of Automatic Landing Controller Using Quantitative Feedback Theory 2016
Lower Bounding Linear Program for the Perimeter Patrol Optimization Problem 2014
Constraint-Monitoring Estimation Strategies for Dynamic Systems Subject to Equality Constraints 2013
Object Correlation, Maneuver Detection, and Characterization Using Control-Distance Metrics 2012
Touch points in optimal ascent trajectories with first-order state inequality constraints 2012
Optimal Formation Design for Magnetospheric Multiscale Mission Using Differential Orbital Elements 2011
Underweighting Nonlinear Measurements 2010
Control Model for Robotic Samara: Dynamics About a Coordinated Helical Turn 2010
Polynomial Chaos-Based Analysis of Probabilistic Uncertainty in Hypersonic Flight Dynamics 2010
Time-Varying Eigensystem Realization Algorithm 2010
Multibody Model of an Ornithopter 2009
Correlation of Optical Observations of Objects in Earth Orbit 2009
Application of the Cayley form to general spacecraft motion 2006
Optimal servicing of geosynchronous satellites 2006
Vision-based sensor and navigation system for autonomous air refueling 2005
Hybrid Cartesian and orbit element feedback law for formation flying spacecraft 2002
Adventures on the interface of dynamics and control 1997
Lyapunov optimal saturated control for nonlinear systems 1997
IDENTIFICATION OF VIBRATING FLEXIBLE STRUCTURES 1985

Journal of Guidance, Control, and Dynamics Journal

Overview

publication venue for

Identity

International Standard Serial Number (ISSN)