Phase coherent Kinematic applications, such as
attitude determination, survey, and phased array multiple antenna systems, place extreme requirements on the
Constellation Simulator hardware and controlling software.
For multiple RF outputs with common satellites on each RF, precise control
of the initial value for carrier phase as well as the relative
value is required. The X14-DSPM and Tapestry controlling software have
collectively solved this problem by implementation of our combined digital
signal with a common RF up-conversion stage the avoids the uncertainty of the initial carrier phase value. We have tested
this system in a 4-RF configuration with a Trimble ADS system and the results
were excellent. Our Tapestry software provides the following features which support
multiple RF output carrier phase applications.
·
The Tapestry system allows for the creation of two vehicles
simultaneously within one scenario. The two vehicle motion profiles can be
completely independent with each vehicle modeled to its own separate RF output.
In this system one vehicle can be dynamic and the other stationary (base station)
or both vehicles can be dynamic. Our software automatically manages the GPS uploads
and satellite selection independently for both modeled vehicles.
·
We have constructed an 8 RF output system in which we have mapped
each satellite to a separate RF output. This system has been used as input to a
wave-front delay matrix for injection into a Controlled Reception Pattern (CRPA)
antenna system. We are in the process of incorporating all of the phase-delay
matrix elements within our system.
·
4-antenna lever arms. These are defined in the vehicle BODY frame
with both position offsets from the vehicle center-of-mass as well as the
capability to define the cone-angle, and orientation of the main antenna beam
lobe. The antenna motion
experienced under dynamics is fully modeled by the Tapestry software
continuous through angular jerk. Our system includes a terrestrial and spaceborn
6-DOF motion generator that includes full attitude maneuvering. Included
is
mutli-element satellite selection algorithm. The
user can either force common satellites on each antenna element or configure
each antenna independently. This was extremely useful for a spaceborn
application in which the spacecraft was rotating a 1 rev/min with 4 antenna
elements spaced 90o apart in look angle. In this case we selected new
satellites every 5 seconds independently on each antenna element as there was
minimal common sky coverage. 4-element vehicle silhouette
masks are provided. The user may
develop independent vehicle silhouette effects for each antenna. These masks are
1o x 1o (default
is 5 o x 5 o) with both upper and lower hemisphere
patterns.
Navigation Laboratories Inc. (949)
766-0444, (949) 495-9551, Fax (949) 713-2479