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| Preface | p. vii |
| Keynote Lecture | p. 1 |
| How Nonlinear Is It?--A Tutorial on Nonlinearity of Orbit and Attitude Dynamics (AAS 03-286) | p. 3 |
| Optimization and Attitude Control | p. 53 |
| Generalized Gradient Search and Newton's Methods for Multilinear Algebra Root-Solving and Optimization Applications (AAS 03-261) | p. 55 |
| Optimal Attitude Control for Coplanar Orbit Phasing Transfers (AAS 03-262) | p. 79 |
| The Attitude Control Problem, Re-Visited (AAS 03-263) | p. 95 |
| Attitude Estimation | p. 111 |
| Attitude Estimation or Quaternion Estimation? (AAS 03-264) | p. 113 |
| Ortho-Skew and Ortho-Sym Matrix Trigonometry (AAS 03-265) | p. 129 |
| Real Time Attitude Independent GPS Integer Ambiguity Resolution (AAS 03-266) | p. 145 |
| Reliable Star Pattern Identification Technique by Using Neural Networks (AAS 03-267) | p. 165 |
| Imaging, Robotics, and Proximity Operations | p. 177 |
| Three-Axis Attitude Simulators for Bifocal Relay Mirror Spacecraft (AAS 03-268) | p. 179 |
| Advances in Imaging System Architectures Through Entry Pupil Processing (AAS 03-269) | p. 193 |
| Enabling Robot Control in Space (AAS 03-270) | p. 213 |
| Stability and Control of Collective Systems (AAS 03-271) | p. 223 |
| NRL Technologies for Autonomous Inter-Space Rendezvous and Proximity Operations (AAS 03-272) | p. 233 |
| Orbits and Trajectory Optimization | p. 251 |
| Taking Heat (AAS 03-273) | p. 253 |
| The Flower Constellations (AAS 03-274) | p. 269 |
| Planetary Capture Using Constant Specific Impulse and Variable Power Propulsion (AAS 03-275) | p. 291 |
| Orbit and Attitude Dynamics, Formation Flying, and Adaptive Control | p. 309 |
| Orbital Motion of Tethered Satellite Systems (AAS 03-276) | p. 311 |
| Modeling and Control of Satellite Formations in High Eccentricity Orbits (AAS 03-277) | p. 325 |
| Challenges and Prospects of Coulomb Spacecraft Formations (AAS 03-278) | p. 351 |
| Adaptive Control--A Departure from the Certainty-Equivalence Paradigm (AAS 03-279) | p. 371 |
| Variable Structure Control With Optimized Sliding Surface for Slew Maneuver (AAS 03-280) | p. 385 |
| Orbit and Attitude Determination, Dynamics, and Numerical Methods | p. 397 |
| Automated Operational Orbit Determination for the ICESat Mission (AAS 03-281) | p. 399 |
| Precision Orbit and Attitude Determination for ICESat (AAS 03-282) | p. 415 |
| Hamel Coefficients for the Rotational Motion of a Rigid Body (AAS 03-283) | p. 427 |
| The Accurate Element Method: A Novel Method for Integrating Ordinary Differential Equations (AAS 03-284) | p. 445 |
| Overview of Star Tracker Technology and its Trends in Research and Development (AAS 03-285) | p. 461 |
| A Low Cost Solid State GPS/INS Attitude Determination System (AAS 03-287) | p. 479 |
| An Efficient and Robust Singular Value Method for Star Pattern Recognition and Attitude Determination (AAS 03-288) | p. 491 |
| Appendices | p. 505 |
| Publications of the American Astronautical Society | p. 506 |
| Advances in the Astronautical Sciences | p. 507 |
| Science and Technology Series | p. 515 |
| AAS History Series | p. 522 |
| Index | p. 525 |
| Numerical Index | p. 527 |
| Author Index | p. 529 |
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