- FUNDAMENTAL RELATION OF APPROXIMATE RECEDING-HORIZON OPTIMIZATION TO THE SIMPLE MASS-SPRING-DAMPER SYSTEM
- Attitude determination designs for the GOES spacecraft John L. Crassidis, F. Landis Markley, Arthur M. Kyle
- OPTIMAL INTEGER RESOLUTION FOR ATTITUDE DETERMINATION USING
- Colored-Noise Kalman Filter for Vibration Mitigation of Position/Attitude Estimation Systems
- Generalizations of the Complex-Step Derivative Approximation
- Paper AAS 02-101 Attitude Determination and Autonomous
- PREDICTIVE FILTERING FOR ATTITUDE ESTIMATION WITHOUT RATE SENSORS
- Multiple Model Adaptive Estimation for Inertial Navigation During Mars Entry
- American Institute of Aeronautics and Astronautics Evaluation of a Multiple Model Adaptive Estimation Scheme
- Kalman Filtering for Relative Inertial Navigation of Uninhabited Air Vehicles
- Convergence Properties of Autocorrelation-Based Generalized Multiple-Model Adaptive Estimation
- ATTITUDE DETERMINATION IMPROVEMENTS FOR GOES John L. Crassidis
- American Institute of Aeronautics and Astronautics APPLICATION OF VECTORIZED ATTITUDE DETERMINATION
- Nonlinear Attitude Filtering Methods F. Landis Markley
- Observability Analysis of Six Degree of Freedom Configuration Determination Using
- Sigma-Point Kalman Filtering for Integrated GPS and Inertial Navigation
- AIAA-2000-3936 AUTONOMOUS ORBIT NAVIGATION OF
- Real-Time Attitude-Independent Three-Axis Magnetometer Calibration
- Generalized Multiple-Model Adaptive Estimation Using an Autocorrelation Approach
- Robust Control of Nonlinear Systems Using Model-Error Control Synthesis
- Paper AAS 00-268 OPTIMAL ATTITUDE AND POSITION
- Stochastic Disturbance Accommodating Control Using a Kalman Estimator
- Robust Aircraft Longitudinal Control Using Model-Error Control Synthesis
- American Institute of Aeronautics and Astronautics FAST INTEGER AMBIGUITY RESOLUTION
- Unscented Filtering for Spacecraft Attitude Estimation
- AIAA-2001-4272 ISS LEAK LOCALIZATION USING
- Extensions of the First and Second Complex-Step Derivative Approximations
- AN EXPECTATION-MAXIMIZATION APPROACH TO ATTITUDE SENSOR CALIBRATION
- Averaging Quaternions F. Landis Markley
- A Survey of Nonlinear Attitude Estimation Methods John L. Crassidis
- Kalman Filtering for Relative Spacecraft Attitude and Position Estimation
- Sensitivity Analysis of Disturbance Accommodating Control with Kalman Filter Estimation
- Second-Order Divided-Difference Filter Using a Generalized Complex-Step Approximation
- Precision Attitude Determination Using a Multiple Model Adaptive Estimation Scheme
- AVERAGING QUATERNIONS , F. Landis Markley
- A Robust GPS Receiver Self Survey Algorithm Keunjoo Park
- Spacecraft Attitude Control Using Approximate Receding-Horizon Model-Error Control Synthesis
- Sigma-Point Kalman Filtering for Integrated GPS and Inertial Navigation
- Kalman Filtering for Relative Spacecraft Attitude and Position Estimation
- Fast Star Pattern Recognition Using Spherical Triangles
- Potential Functions for En-Route Air Traffic Management and Flight Planning
- Particle Filtering for Sequential Spacecraft Attitude Estimation
- AUTONOMOUS ORBIT NAVIGATION OF TWO SPACECRAFT SYSTEM USING RELATIVE LINE OF SIGHT
- Applied Linear Optimal Control: Examples and Algorithms Arthur E. Bryson, Cambridge University Press, United Kingdom, 2002, 362
- IN-SPACE SPACECRAFT ALIGNMENT CALIBRATION USING THE UNSCENTED FILTER
- ROBUST SPACECRAFT ATTITUDE CONTROL USING MODEL-ERROR CONTROL SYNTHESIS
- ATTITUDE DETERMINATION USING COMBINED GPS AND THREE-AXIS
- AIAA-2001-4220 MODEL-ERROR CONTROL SYNTHESIS USING
- RELATIVE NAVIGATION FOR FORMATION FLYING OF SPACECRAFT
- Optimal Attitude and Position Determination from Line-of-Sight
- H Control of Active Constrained Layer Damping JOHN L. CRASSIDIS
- AIAA-2000-4439 VISION-BASED RELATIVE NAVIGATION
- ROBUST CONTROL OF NONLINEAR SYSTEMS USING MODEL-ERROR CONTROL SYNTHESIS
- Autonomous Attitude Determination for ISS Applications Using Pseudolite Signals
- American Institute of Aeronautics and Astronautics A NOVEL SENSOR FOR ATTITUDE DETERMINATION USING
- Nonlinear Predictive Control of Spacecraft John L. Crassidis1
- A New Algorithm for Attitude Determination Using Global Positioning System Signals
- Predictive Filtering for Nonlinear Systems John L. Crassidis1
- American Institute of Aeronautics and Astronautics ATTITUDE DETERMINATION USING GLOBAL
- Predictive Attitude Estimation Using Global Positioning System Signals
- A Predictive Attitude Determination Algorithm John L. Crassidis
- A Minimum Model Error Approach for Attitude Estimation John L. Crassidis
- CONTINGENCY DESIGNS FOR ATTITUDE DETERMINATION OF TRMM
- F. Landis Markley Francis Landis Markley, Jr., was born in Philadelphia, Pennsylvania, on July 20,
- F. Landis Markley Selected Publications In Astronautics
- Call for Papers F. Landis Markley Astronautics Symposium
- 2:50 3:15 [05-476] "Analysis of Trajectories to Neptune Using Gravity Assists," C. R. Solrzano, A. A. Sukhanov and A. F. Prado
- BY INVITATION ONLY DO NOT POST Call for Papers
- FORMAT INSTRUCTIONS FOR AAS TECHNICAL PAPERS* Robert H. Jacobs
- American Institute of Aeronautics and Astronautics AIAA-98-4496
- Malcolm D. Shuster Selected Publications in Astronautics*
- AIAA-2000-3963 LINEAR STABILITY ANALYSIS OF
- Ground Target Tracking Using Terrain Information
- Relative Navigation of Air Vehicles Adam M. Fosbury
- LIMIT CYCLE OSCILLATION CONTROL OF AEROELASTIC SYSTEM USING MODEL-ERROR CONTROL SYNTHESIS
- American Institute of Aeronautics and Astronautics NONLINEAR PREDICTIVE CONTROL OF SPACECRAFT
- REAL-TIME ATTITUDE-INDEPENDENT THREE-AXIS MAGNETOMETER CALIBRATION
- A Minimum Model Error Approach for Attitude Estimation John L. Crassidis1
- Deterministic Relative Attitude Determination of Formation Flying Spacecraft
- Fast Star Pattern Recognition Using Planar Triangles
- AAS Astrodynamics Symposium, Grand Island, New York, June 1315 2005 Welcoming Remarks
- 58th International Astronautical Congress 2007 Frank J. Centinello III
- Angular Velocity Determination Directly from Star Tracker Measurements
- LINEARIZING ASSUMPTIONS AND CONTROL DESIGN FOR SPACECRAFT FORMATION FLYING MANEUVERS
- Nonlinear Filtering Based On Sequential Model Error Determination
- International Space Station Leak Localization Using Attitude Disturbance Estimation
- Micro-arcsecond Line-of-Sight Filtered Performance for Spacecraft Formation Flying
- Efficient and Optimal Attitude Determination Using Recursive Global Positioning System
- American Institute of Aeronautics and Astronautics PREDICTIVE FILTERING FOR NONLINEAR SYSTEMS
- New Complex-Step Derivative Approximations with Application to Second-Order Kalman Filtering
- Optimal Trajectory Determination for Increased Relative Navigation Observability of Air Vehicles
- AN MME-BASED ATTITUDE ESTIMATOR USING VECTOR OBSERVATIONS
- UNSCENTED FILTERING FOR SPACECRAFT ATTITUDE ESTIMATION
- ATTITUDE ESTIMATION FOR LARGE FIELD-OF-VIEW SENSORS
- International Space Station Leak Localization Using Attitude Response Data
- Real-Time Attitude-Independent Gyro Calibration from Three-Axis Magnetometer Measurements
- THE MALCOLM D. SHUSTER ASTRONAUTICS SYMPOSIUM
- Mercedes Arribas University of Zaragoza marribas@unizar.es Peter M. Bainum Howard University pbainum@howard.edu
- Book Corrections for Optimal Estimation of Dynamic Systems
- Predictive Filtering for Attitude Estimation Without Rate Sensors
- SPACECRAFT ANGULAR RATE ESTIMATION ALGORITHMS FOR STAR TRACKER-BASED ATTITUDE DETERMINATION
- DECENTRALIZED ATTITUDE ESTIMATION USING A QUATERNION COVARIANCE INTERSECTION APPROACH
- Attitude Estimation for Large Field-of-View Sensors , John L. Crassidis
- Real Time Attitude Independent GPS Integer Ambiguity Resolution
- Attitude Determination Methods Using Pseudolite Signal Phase Measurements
- IAC-04-A.4.10 INTERNATIONAL SPACE STATION LEAK
- REAL TIME ATTITUDE INDEPENDENT GPS INTEGER AMBIGUITY RESOLUTION
- Global Positioning System Integer Ambiguity Resolution without Attitude Knowledge
- Malcolm D. Shuster Malcolm D. Shuster was born in Boston, Massachusetts, on July 31, 1943, and spent his for-
- OPTIMAL VARIABLE-STRUCTURE CONTROL TRACKING OF SPACECRAFT MANEUVERS
- Spacecraft Attitude Control Using Approximate Receding-Horizon Model-Error Control Synthesis
- Book Corrections for Optimal Estimation of Dynamic Systems, 2nd
