Review of Attitude Representations Used for Aircraft Kinematics
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[1] R. G. Reynolds. QUATERNION PARAMETERIZATION AND A SIMPLE ALGORITHM FOR GLOBAL ATTITUDE ESTIMATION , 1998 .
[2] Jack B. Kuipers. SPASYN-an electromagnetic relative position and orientation tracking system , 1980, IEEE Transactions on Instrumentation and Measurement.
[3] Thor I. Fossen,et al. Position and attitude tracking of AUV's: a quaternion feedback approach , 1994 .
[4] John L. Junkins,et al. Analytical solutions for Euler parameters , 1974 .
[5] Nathan C. Prewitt,et al. Multiple-Body Trajectory Calculations Using the Beggar Code , 1999 .
[6] Kostas Daniilidis,et al. Hand-Eye Calibration Using Dual Quaternions , 1999, Int. J. Robotics Res..
[7] S. Winograd. On the number of multiplications necessary to compute certain functions , 1970 .
[8] Robert C. Nelson,et al. Flight Stability and Automatic Control , 1989 .
[9] R. Roberson. Kinematical equations for bodies whose rotation is described by the Euler-Rodrigues parameter. , 1968 .
[10] William J Thome. Quaternion Utilization in a Missile Model , 1980 .
[11] R. Mortensen. Strapdown Guidance Error Analysis , 1974, IEEE Transactions on Aerospace and Electronic Systems.
[12] J. Pieper,et al. Error analysis of direction cosines and quaternion parameters techniques for aircraft attitude determination , 1998 .
[13] DERIVATION OF THE EQUATIONS OF MOTION OF A CLASSICAL RADIATING CHARGE. , 1967 .
[14] Marcel J. Sidi,et al. Attitude Transformations in Space , 1997 .
[15] Finite Rotations and Associated Displacement Vectors , 1976 .
[16] William Rowan Hamilton,et al. LXXVIII. On quaternions; or on a new system of imaginaries in Algebra: To the editors of the Philosophical Magazine and Journal , 1844 .
[17] Christopher D. Hall,et al. Spacecraft Dynamics and Control , 2002 .
[18] C. Grubin. Derivation of the quaternion scheme via the Euler axis and angle , 1970 .
[19] Fadi Dornaika,et al. Simultaneous robot-world and hand-eye calibration , 1998, IEEE Trans. Robotics Autom..
[20] A. W. Babister. Aircraft stability and control , 1961 .
[21] William Rowan Hamilton,et al. Elements of Quaternions , 1969 .
[22] Arthur Mayer,et al. ROTATIONS AND THEIR ALGEBRA , 1960 .
[23] Allan R. Klumpp. Reply by Author to R.A. Spurrier , 1978 .
[24] J. Wen,et al. Robust attitude stabilization of spacecraft using nonlinear quaternion feedback , 1995, IEEE Trans. Autom. Control..
[25] John L. Junkins,et al. New results on the optimal spacecraft attitude maneuver problem , 1984 .
[26] J. Bortz. A New Mathematical Formulation for Strapdown Inertial Navigation , 1971, IEEE Transactions on Aerospace and Electronic Systems.
[27] M. V. Cook. Flight Dynamics Principles , 1997 .
[28] Haim Weiss,et al. Quarternion feedback regulator for spacecraft eigenaxis rotations , 1989 .
[29] Roger A. Broucke. On the use of poincare surfaces of section in rigid-body motion , 1993 .
[30] W. F. Phillips,et al. Aircraft small-disturbance theory with longitudinal-lateral coupling , 2002 .
[31] Jackson E. Bruce. Manual for a Workstation-Based Generic Flight Simulation Program (LaRCsim) Version 1.4 , 1995 .
[32] H. S. Ribner,et al. Wake Forces Implied in the Theodorsen and Goldstein Theories of Propellers , 1998 .
[33] Yeon Fuh Jiang,et al. Error analysis of quaternion transformations (inertial navigation) , 1991 .
[34] Ammon Katz,et al. Special rotation vectors - A means for transmitting quaternions in three components , 1993 .
[35] R. A. Mayo. Relative Quaternion State Transition Relation , 1979 .
[36] Stanley W. Shepperd,et al. Quaternion from Rotation Matrix , 1978 .
[37] H. C. Corben,et al. Classical Mechanics (2nd ed.) , 1961 .
[38] Andrew J. Hanson,et al. Quaternion Frame Approach to Streamline Visualization , 1995, IEEE Trans. Vis. Comput. Graph..
[39] Carl B. Boyer,et al. A History of Mathematics. , 1993 .
[40] R. A. Spurrier. Comment on " Singularity-Free Extraction of a Quaternion from a Direction-Cosine Matrix" , 1978 .
[41] L. E. Miller,et al. Use of Quaternions in Flight Mechanics , 1984 .
[42] J. Kuipers. Quaternions and Rotation Sequences , 1998 .
[43] J.C.K. Chou,et al. Quaternion kinematic and dynamic differential equations , 1992, IEEE Trans. Robotics Autom..
[44] K. C. Gupta,et al. An historical note on finite rotations , 1989 .
[45] Itzhack Y. Bar-Itzhack,et al. Iterative computation of initial quaternion , 1970 .
[46] Liang-Boon Wee,et al. An articulated-body model for a free-flying robot and its use for adaptive motion control , 1997, IEEE Trans. Robotics Autom..
[47] Jeremy Gray,et al. Olinde Rodrigues' paper of 1840 on transformation groups , 1980 .
[48] Itzhack Y. Bar-itzhack,et al. Optimum Normalization of a Computed Quaternion of Rotation , 1971, IEEE Transactions on Aerospace and Electronic Systems.
[49] J. M. Rolfe,et al. Flight simulation , 1988 .
[50] Chan Gook Park,et al. Strapdown INS error model for multiposition alignment , 1996 .
[51] Bruno Siciliano,et al. Six-DOF impedance control based on angle/axis representations , 1999, IEEE Trans. Robotics Autom..
[52] James C. Wilcox,et al. A New Algorithm for Strapped-Down Inertial Navigation , 1967, IEEE Transactions on Aerospace and Electronic Systems.
[53] Paul DeLaHunt,et al. ATTITUDE DETERMINATION AND CONTROL OF CLEMENTINE DURING LUNAR MAPPING , 1996 .
[54] Roger A. Wehage. Quaternions and Euler Parameters — A Brief Exposition , 1984 .
[55] A. R. Klumpp,et al. Singularity-free extraction of a quaternion from a direction-cosine matrix. [for spacecraft control and guidance] , 1976 .
[56] Richard L. Pio. Symbolic Representation of Coordinate Transformations , 1964, IEEE Transactions on Aerospace and Navigational Electronics.
[57] Duane T. McRuer,et al. Aircraft Dynamics and Automatic Control , 1973 .
[58] E. Wilson,et al. To the Finland Station , 1940 .
[59] J. Stuelpnagel. On the Parametrization of the Three-Dimensional Rotation Group , 1964 .
[60] Franz S. Hover,et al. Simulation of stiff massless tethers , 1997 .
[61] I. Bar-Itzhack. REQUEST: A Recursive QUEST Algorithm for Sequential Attitude Determination , 1996 .
[62] J. Hoffman. Numerical Methods for Engineers and Scientists , 2018 .
[63] Coordinate‐free rotation formalism , 1976 .
[64] A. G. Kelkar,et al. Global stabilization of flexible multibody spacecraft using quaternion-based nonlinear control law , 1996 .
[65] A. E. Sabroff,et al. INVESTIGATION OF THE ACQUISITION PROBLEM IN SATELLITE ATTITUDE CONTROL. , 1965 .
[66] Lioudmila I. Aramanovitch. Spacecraft orientation based on space object observations by means of quaternion algebra , 1995 .
[67] D. I. Kolve. Describing an attitude , 1993 .
[68] A. E. Rogers,et al. Quaternion Parameters in the Simulation of a Spinning Rigid Body , 1965 .
[69] Michael G. Crowe,et al. A History of Vector Analysis , 1969 .
[70] David A. Pope. An exponential method of numerical integration of ordinary differential equations , 1963, CACM.
[71] Bernard Etkin,et al. Dynamics of Atmospheric Flight , 1972 .
[72] B. Ickes. A new method for performing digital control system attitude computations using quaternions , 1970 .
[73] Optimal Control of Quaternion Propagation Errors in Spacecraft Navigation , 1986 .
[74] D. J. Winter. A History of Algebra. , 1988 .
[75] Malcolm J. Abzug. Computational Flight Dynamics , 1998 .
[76] W. Phillips,et al. A Review of Attitude Kinematics for Aircraft Flight Simulation , 2000 .
[77] Penny Probert Smith,et al. A Sensor System for the Navigation of an Underwater Vehicle , 1999, Int. J. Robotics Res..
[78] P. Hughes. Spacecraft Attitude Dynamics , 1986 .
[79] B. Friedland. Analysis Strapdown Navigation Using Quaternions , 1978, IEEE Transactions on Aerospace and Electronic Systems.
[80] Millard F. Beatty,et al. Kinematics of Finite, Rigid-Body Displacements , 1966 .
[81] Moshe Idan,et al. Recursive attitude determination from vector observations Euler angle estimation , 1987 .
[82] M. Shuster. A survey of attitude representation , 1993 .
[83] I. Satake,et al. Linear algebra , 1975 .
[84] Jang Gyu Lee,et al. Comparison of SDINS in-flight alignment using equivalent error models , 1999 .
[85] M. Kaplan. Modern Spacecraft Dynamics and Control , 1976 .
[86] Jack C. K. Chou,et al. Finding the Position and Orientation of a Sensor on a Robot Manipulator Using Quaternions , 1991, Int. J. Robotics Res..
[87] J. W. Humberston. Classical mechanics , 1980, Nature.
[88] A. Messiah. Quantum Mechanics , 1961 .
[89] C. Grubin,et al. Attitude determination for a strapdown inertial system using the Euler axis/angle and quaternion parameters , 1973 .
[90] T. Teichmann,et al. Dynamics of Flight: Stability and Control , 1959 .
[91] Chan Gook Park,et al. Modeling quaternion errors in SDINS: computer frame approach , 1998 .
[92] Millard F. Beatty,et al. Vector Representation of Rigid Body Rotation , 1963 .
[93] B. L. Waerden,et al. A history of algebra : from Al-Khwārizmī to Emmy Noether , 1985 .
[94] C. Grubin. Vector Representation of Rigid Body Rotation , 1962 .
[95] S. Gupta,et al. Linear quaternion equations with application to spacecraft attitude propagation , 1998, 1998 IEEE Aerospace Conference Proceedings (Cat. No.98TH8339).
[96] S. Altmann,et al. Hamilton, Rodrigues, and the Quaternion Scandal , 1989 .
[97] W. F. Phillips,et al. Analytical Approximation for the Mechanics of Airplane Spin , 2002 .
[98] Aiichiro Nakano,et al. A Rigid-Body-Based Multiple Time Scale Molecular Dynamics Simulation of Nanophase Materials , 1999, Int. J. High Perform. Comput. Appl..
[99] Gano B. Chatterji,et al. A Quaternion Formulation for Boost Phase Attitude Estimation, Guidance and Control of Exoatmospheric Interceptors , 1989, 1989 American Control Conference.
[100] R. Pio. Euler angle transformations , 1966 .
[101] Edmund Taylor Whittaker,et al. A Treatise on the Analytical Dynamics of Particles and Rigid Bodies: THE GENERAL THEORY OF ORBITS , 1988 .
[102] E. J. Lefferts,et al. Kalman Filtering for Spacecraft Attitude Estimation , 1982 .
[103] S. Vathsal,et al. Derivation of the relative quaternion differential equation , 1991 .
[104] M. Beatty. Vector Analysis of Finite Rigid Rotations , 1977 .
[105] Shih-Che Lo,et al. Smooth Sliding-Mode Control for Spacecraft Attitude Tracking Maneuvers , 1995 .
[106] Richard A McKern,et al. A study of transformation algorithms for use in a digital computer. , 1968 .
[107] Arthur W. Babister,et al. Aircraft dynamic stability and response , 1980 .
[108] C. Grubin. Quaternion Singularity Revisited , 1979 .
[109] Nathan C. Prewitt,et al. Multiple body trajectory calculations using the Beggar code , 1996 .
[110] Vector Representation of Rigid-Body Rotation , 1967 .
[111] I. Bar-Itzhack,et al. Attitude Determination from Vector Observations: Quaternion Estimation , 1985, IEEE Transactions on Aerospace and Electronic Systems.
[112] V. N. Dvornychenko. The number of multiplications required to chain coordinate transformations , 1985 .
[113] G. Cook,et al. Improved Local Linearization Algorithm for Solving the Quaternion Equations , 1980 .
[114] Robert E. Hage,et al. Airplane Performance, Stability and Control , 1949 .
[115] A. W. Babister. Chapter 2 – THE EQUATIONS OF MOTION , 1980 .
[116] C. C. Macduffee,et al. The Theory of Matrices , 1933 .
[117] Ken Shoemake,et al. Animating rotation with quaternion curves , 1985, SIGGRAPH.
[118] John L. Crassidis,et al. Sliding Mode Control Using Modified Rodrigues Parameters , 1996 .
[119] Greg Welch,et al. An Introduction to Kalman Filter , 1995, SIGGRAPH 2001.
[120] Igor P. Omelyan. On the numerical integration of motion for rigid polyatomics: the modified quaternion approach , 1998 .
[121] C. E. Hailey,et al. The effects of orthogonality error in aircraft flight simulation , 2001 .
[122] John C. Hart,et al. Visualizing quaternion rotation , 1994, TOGS.
[123] R. Graves,et al. The Life of Sir William Rowan Hamilton , 1889, Nature.