Strapdown inertial navigation integration algorithm design Part 2: Velocity and position algorithms

被引:259
作者
Savage, PG [1 ]
机构
[1] Strapdown Associates Inc, Maple Plain, MN 55359 USA
关键词
D O I
10.2514/2.4242
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This series of two papers (Parts 1 and 2) provides a rigorous comprehensive approach to the design of the principal software algorithms utilized in modern-day strapdown inertial navigation systems: integration of angular rate into attitude, acceleration transformation/integration into velocity, and integration of velocity into position. The algorithms are structured utilizing the two-speed updating approach originally developed for attitude updating; an analytically exact equation is used a moderate speed to update the integration parameter (attitude, velocity, or po sition) with input provided from sr high-speed algorithm measuring rectified dynamic motion within the parameter update time interval [coming far attitude updating, sculling for velocity updating, and scrolling (writer's terminology) for high-resolution position updating]. The algorithm design approach accounts for angular rate/specific force acceleration inputs from the strapdown system inertial sensors, as well as rotation of the navigation frame used for attitude referencing and velocity integration. The Pare 1 paper (Savage, P. G., "Strapdown Inertial Navigation Integration Algorithm Design Part 1: Attitude Algorithms," Journal of Guidance Control, and Dynamics, Vol. 21, No, 1, 1998, pip 19-28) defined the overall design requirement for the strapdown inertial navigation integration function and developed the attitude updating algorithms. This paper, Part 2, deals with design of the acceleration transformation/velocity integration and position integration algorithms. Although Parts I and 2 often cover basic concepts, the material presented is intended for use by the practitioner who is already familiar with inertial navigation fundamentals.
引用
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页码:208 / 221
页数:14
相关论文
共 11 条
[2]   Efficient class of optimized coning compensation algorithms [J].
Ignagni, MB .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (02) :424-429
[3]   OPTIMAL STRAPDOWN ATTITUDE INTEGRATION ALGORITHMS [J].
IGNAGNI, MB .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1990, 13 (02) :363-369
[4]  
Jordan J. W., 1969, TND5384 NASA
[5]  
MARK JG, 1996, 3 ST PET INT C INT N
[6]   A NEW STRAPDOWN ATTITUDE ALGORITHM [J].
MILLER, RB .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1983, 6 (04) :287-291
[7]  
Savage P., 1997, INTRO STRAPDOWN INER
[8]  
Savage P., AIAA JACC GUID CONTR
[9]  
Savage P.G., 1984, NATO AGARD LECT SERI
[10]   Strapdown inertial navigation integration algorithm design part 1: Attitude algorithms [J].
Savage, PG .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1998, 21 (01) :19-28