gftfov_c |

## Procedurevoid gftfov_c ( ConstSpiceChar * inst, ConstSpiceChar * target, ConstSpiceChar * tshape, ConstSpiceChar * tframe, ConstSpiceChar * abcorr, ConstSpiceChar * obsrvr, SpiceDouble step, SpiceCell * cnfine, SpiceCell * result ) ## AbstractDetermine time intervals when a specified ephemeris object intersects the space bounded by the field-of-view (FOV) of a specified instrument. ## Required_ReadingCK FRAMES GF KERNEL NAIF_IDS PCK SPK TIME WINDOWS ## KeywordsEVENT FOV GEOMETRY INSTRUMENT SEARCH WINDOW ## Brief_I/OVARIABLE I/O DESCRIPTION --------------- --- ------------------------------------------------ SPICE_GF_MARGIN P Minimum complement of FOV cone angle. SPICE_GF_CNVTOL P Convergence tolerance. SPICE_GF_MAXVRT P Maximum number of FOV boundary vertices. inst I Name of the instrument. target I Name of the target body. tshape I Type of shape model used for target body. tframe I Body-fixed, body-centered frame for target body. abcorr I Aberration correction flag. obsrvr I Name of the observing body. step I Step size in seconds for finding FOV events. cnfine I-O SPICE window to which the search is restricted. result O SPICE window containing results. ## Detailed_Inputinst indicates the name of an instrument, such as a spacecraft-mounted framing camera, the field of view (FOV) of which is to be used for a target intersection search: times when the specified target intersects the region of space corresponding to the FOV are sought. The position of the instrument designated by `inst' is considered to coincide with that of the ephemeris object designated by the input argument `obsrvr' (see description below). `inst' must have a corresponding NAIF ID and a frame defined, as is normally done in a frame kernel. It must also have an associated reference frame and a FOV shape, boresight and boundary vertices (or reference vector and reference angles) defined, as is usually done in an instrument kernel. See the header of the CSPICE routine getfov_c for a description of the required parameters associated with an instrument. target is the name of the target body, the appearances of which in the specified instrument's field of view are sought. The body must be an ephemeris object. Optionally, you may supply the integer NAIF ID code for the body as a string. For example both "MOON" and "301" are legitimate strings that designate the Moon. Case and leading or trailing blanks are not significant in the string `target'. tshape is a string indicating the geometric model used to represent the shape of the target body. The supported options are: "ELLIPSOID" Use a triaxial ellipsoid model, with radius values provided via the kernel pool. A kernel variable having a name of the form "BODYnnn_RADII" where nnn represents the NAIF integer code associated with the body, must be present in the kernel pool. This variable must be associated with three numeric values giving the lengths of the ellipsoid's X, Y, and Z semi-axes. "POINT" Treat the body as a single point. Case and leading or trailing blanks are not significant in the string `tshape'. tframe is the name of the body-fixed, body-centered reference frame associated with the target body. Examples of such names are "IAU_SATURN" (for Saturn) and "ITRF93" (for the Earth). If the target body is modeled as a point, `tframe' is ignored and should be left blank. Case and leading or trailing blanks bracketing a non-blank frame name are not significant in the string `tframe'. abcorr indicates the aberration corrections to be applied when computing the target's position and orientation. For remote sensing applications, where the apparent position and orientation of the target seen by the observer are desired, normally either of the corrections "LT+S" "CN+S" should be used. These and the other supported options are described below. Supported aberration correction options for observation (the case where radiation is received by observer at ET) are: "NONE" No correction. "LT" Light time only "LT+S" Light time and stellar aberration. "CN" Converged Newtonian (CN) light time. "CN+S" CN light time and stellar aberration. Supported aberration correction options for transmission (the case where radiation is emitted from observer at ET) are: "XLT" Light time only. "XLT+S" Light time and stellar aberration. "XCN" Converged Newtonian (CN) light time. "XCN+S" CN light time and stellar aberration. For detailed information, see the GF Required Reading, gf.req. Case, leading and trailing blanks are not significant in the string `abcorr'. obsrvr is the name of the body from which the target is observed. The instrument designated by `inst' is treated as if it were co-located with the observer. Optionally, you may supply the integer NAIF ID code for the body as a string. Case and leading or trailing blanks are not significant in the string `obsrvr'. step is the step size to be used in the search. `step' must be shorter than any interval, within the confinement window, over which the specified condition is met. In other words, `step' must be shorter than the shortest visibility event that the user wishes to detect. `step' also must be shorter than the minimum duration separating any two visibility events. However, `step' must not be *too* short, or the search will take an unreasonable amount of time. The choice of `step' affects the completeness but not the precision of solutions found by this routine; the precision is controlled by the convergence tolerance. See the discussion of the parameter SPICE_GF_CNVTOL for details. `step' has units of seconds. cnfine is a SPICE window that confines the time period over which the specified search is conducted. `cnfine' may consist of a single interval or a collection of intervals. The endpoints of the time intervals comprising `cnfine' are interpreted as seconds past J2000 TDB. See the Examples section below for a code example that shows how to create a confinement window. ## Detailed_Outputcnfine is the input confinement window, updated if necessary so the control area of its data array indicates the window's size and cardinality. The window data are unchanged. result is a SPICE window representing the set of time intervals, within the confinement period, when the target body is visible; that is, when the target body intersects the space bounded by the specified instrument's field of view. The endpoints of the time intervals comprising `result' are interpreted as seconds past J2000 TDB. If `result' is non-empty on input, its contents will be discarded before ## ParametersAll parameters described here are declared in the header file SpiceGF.h. See that file for parameter values. SPICE_GF_CNVTOL is the convergence tolerance used for finding endpoints of the intervals comprising the result window. SPICE_GF_CNVTOL is used to determine when binary searches for roots should terminate: when a root is bracketed within an interval of length SPICE_GF_CNVTOL, the root is considered to have been found. The accuracy, as opposed to precision, of roots found by this routine depends on the accuracy of the input data. In most cases, the accuracy of solutions will be inferior to their precision. SPICE_GF_MAXVRT is the maximum number of vertices that may be used to define the boundary of the specified instrument's field of view. SPICE_GF_MARGIN is a small positive number used to constrain the orientation of the boundary vectors of polygonal FOVs. Such FOVs must satisfy the following constraints: 1) The boundary vectors must be contained within a right circular cone of angular radius less than than (pi/2) - SPICE_GF_MARGIN radians; in other words, there must be a vector A such that all boundary vectors have angular separation from A of less than (pi/2)-SPICE_GF_MARGIN radians. 2) There must be a pair of boundary vectors U, V such that all other boundary vectors lie in the same half space bounded by the plane containing U and V. Furthermore, all other boundary vectors must have orthogonal projections onto a specific plane normal to this plane (the normal plane contains the angle bisector defined by U and V) such that the projections have angular separation of at least 2*SPICE_GF_MARGIN radians from the plane spanned by U and V. ## Exceptions1) In order for this routine to produce correct results, the step size must be appropriate for the problem at hand. Step sizes that are too large may cause this routine to miss roots; step sizes that are too small may cause this routine to run unacceptably slowly and in some cases, find spurious roots. This routine does not diagnose invalid step sizes, except that if the step size is non-positive, the error SPICE(INVALIDSTEPSIZE) will be signaled. 2) Due to numerical errors, in particular, - Truncation error in time values - Finite tolerance value - Errors in computed geometric quantities it is *normal* for the condition of interest to not always be satisfied near the endpoints of the intervals comprising the result window. The result window may need to be contracted slightly by the caller to achieve desired results. The SPICE window routine WNCOND can be used to contract the result window. 3) If the name of either the target or observer cannot be translated to a NAIF ID code, the error will be diagnosed by a routine in the call tree of this routine. 4) If the specified aberration correction is an unrecognized value, the error will be diagnosed and signaled by a routine in the call tree of this routine. 5) If the radii of a target body modeled as an ellipsoid cannot be determined by searching the kernel pool for a kernel variable having a name of the form "BODYnnn_RADII" where nnn represents the NAIF integer code associated with the body, the error will be diagnosed by a routine in the call tree of this routine. 6) If the target body coincides with the observer body `obsrvr', the error will be diagnosed by a routine in the call tree of this routine. 7) If the body model specifier `tshape' is invalid, the error will be diagnosed either here or by a routine in the call tree of this routine. 8) If a target body-fixed reference frame associated with a non-point target is not recognized, the error will be diagnosed by a routine in the call tree of this routine. 9) If a target body-fixed reference frame is not centered at the corresponding target body, the error will be diagnosed by a routine in the call tree of this routine. 10) If the instrument name `inst' does not have corresponding NAIF ID code, the error will be diagnosed by a routine in the call tree of this routine. 11) If the FOV parameters of the instrument are not present in the kernel pool, the error will be be diagnosed by routines in the call tree of this routine. 12) If the FOV boundary has more than SPICE_GF_MAXVRT vertices, the error will be be diagnosed by routines in the call tree of this routine. 13) If the instrument FOV is polygonal, and this routine cannot find a ray R emanating from the FOV vertex such that maximum angular separation of R and any FOV boundary vector is within the limit (pi/2)-SPICE_GF_MARGIN radians, the error will be diagnosed by a routine in the call tree of this routine. If the FOV is any other shape, the same error check will be applied with the instrument boresight vector serving the role of R. 14) If the loaded kernels provide insufficient data to compute a requested state vector, the error will be diagnosed by a routine in the call tree of this routine. 15) If an error occurs while reading an SPK or other kernel file, the error will be diagnosed by a routine in the call tree of this routine. 16) If the output SPICE window `result' has insufficient capacity to contain the number of intervals on which the specified visibility condition is met, the error will be diagnosed by a routine in the call tree of this routine. If the result window has size less than 2, the error SPICE(WINDOWTOOSMALL) will be signaled by this routine. 17) If any input string argument pointer is null, the error SPICE(NULLPOINTER) will be signaled. 18) If any input string argument other than `tframe' is empty, the error SPICE(EMPTYSTRING) will be signaled. ## FilesAppropriate SPICE kernels must be loaded by the calling program before this routine is called. The following data are required: - SPK data: ephemeris data for target and observer that describes the ephemeris of these objects for the period defined by the confinement window CNFINE must be loaded. If aberration corrections are used, the states of target and observer relative to the solar system barycenter must be calculable from the available ephemeris data. Typically ephemeris data are made available by loading one or more SPK files via furnsh_c. - Frame data: if a frame definition is required to convert the observer and target states to the body-fixed frame of the target, that definition must be available in the kernel pool. Typically the definitions of frames not already built-in to SPICE are supplied by loading a frame kernel. Data defining the reference frame associated with the instrument designated by `inst' must be available in the kernel pool. Additionally the name `inst' must be associated with an ID code. Normally these data are made available by loading a frame kernel via furnsh_c. - IK data: the kernel pool must contain data such that the CSPICE routine getfov_c may be called to obtain parameters for `inst'. Normally such data are provided by an IK via furnsh_c. The following data may be required: - PCK data: bodies modeled as triaxial ellipsoids must have orientation data provided by variables in the kernel pool. Typically these data are made available by loading a text PCK file via furnsh_c. Bodies modeled as triaxial ellipsoids must have semi-axis lengths provided by variables in the kernel pool. Typically these data are made available by loading a text PCK file via furnsh_c. - CK data: if the instrument frame is fixed to a spacecraft, at least one CK file will be needed to permit transformation of vectors between that frame and both J2000 and the target body-fixed frame. - SCLK data: if a CK file is needed, an associated SCLK kernel is required to enable conversion between encoded SCLK (used to time-tag CK data) and barycentric dynamical time (TDB). Kernel data are normally loaded once per program run, NOT every time this routine is called. ## ParticularsThis routine determines a set of one or more time intervals within the confinement window when any portion of a specified target body appears within the field of view of a specified instrument. We'll use the term "visibility event" to designate such an appearance. The set of time intervals resulting from the search is returned as a SPICE window. This routine provides a simpler, but less flexible, interface than does the CSPICE routine gffove_c for conducting searches for visibility events. Applications that require support for progress reporting, interrupt handling, non-default step or refinement functions, or non-default convergence tolerance should call gffove_c rather than this routine. To treat the target as a ray rather than as an ephemeris object, use either the higher-level CSPICE routine gfrfov_c or gffove_c. Those routines may be used to search for times when distant target objects such as stars are visible in an instrument FOV, as long the direction from the observer to the target can be modeled as a ray. Below we discuss in greater detail aspects of this routine's solution process that are relevant to correct and efficient use of this routine in user applications. The Search Process ================== The search for visibility events is treated as a search for state transitions: times are sought when the state of the target body changes from "not visible" to "visible" or vice versa. Step Size ========= Each interval of the confinement window is searched as follows: first, the input step size is used to determine the time separation at which the visibility state will be sampled. Starting at the left endpoint of an interval, samples will be taken at each step. If a state change is detected, a root has been bracketed; at that point, the "root"--the time at which the state change occurs---is found by a refinement process, for example, via binary search. Note that the optimal choice of step size depends on the lengths of the intervals over which the visibility state is constant: the step size should be shorter than the shortest visibility event duration and the shortest period between visibility events, within the confinement window. Having some knowledge of the relative geometry of the target and observer can be a valuable aid in picking a reasonable step size. In general, the user can compensate for lack of such knowledge by picking a very short step size; the cost is increased computation time. Note that the step size is not related to the precision with which the endpoints of the intervals of the result window are computed. That precision level is controlled by the convergence tolerance. Convergence Tolerance ===================== Once a root has been bracketed, a refinement process is used to narrow down the time interval within which the root must lie. This refinement process terminates when the location of the root has been determined to within an error margin called the "convergence tolerance." The convergence tolerance used by this routine is set via the parameter SPICE_GF_CNVTOL. The value of SPICE_GF_CNVTOL is set to a "tight" value so that the tolerance doesn't become the limiting factor in the accuracy of solutions found by this routine. In general the accuracy of input data will be the limiting factor. To use a different tolerance value, a lower-level GF routine such as gffove_c must be called. Making the tolerance tighter than SPICE_GF_CNVTOL is unlikely to be useful, since the results are unlikely to be more accurate. Making the tolerance looser will speed up searches somewhat, since a few convergence steps will be omitted. However, in most cases, the step size is likely to have a much greater effect on processing time than would the convergence tolerance. The Confinement Window ====================== The simplest use of the confinement window is to specify a time interval within which a solution is sought. However, the confinement window can, in some cases, be used to make searches more efficient. Sometimes it's possible to do an efficient search to reduce the size of the time period over which a relatively slow search of interest must be performed. For an example, see the program CASCADE in the GF Example Programs chapter of the GF Required Reading, gf.req. ## ExamplesThe numerical results shown for these examples may differ across platforms. The results depend on the SPICE kernels used as input, the compiler and supporting libraries, and the machine specific arithmetic implementation. 1) Search for times when Saturn's satellite Phoebe is within the FOV of the Cassini narrow angle camera (CASSINI_ISS_NAC). To simplify the problem, restrict the search to a short time period where continuous Cassini bus attitude data are available. Use a step size of 10 seconds to reduce chances of missing short visibility events. Use the meta-kernel shown below to load the required SPICE kernels. KPL/MK File name: gftfov_ex1.tm This meta-kernel is intended to support operation of SPICE example programs. The kernels shown here should not be assumed to contain adequate or correct versions of data required by SPICE-based user applications. In order for an application to use this meta-kernel, the kernels referenced here must be present in the user's current working directory. The names and contents of the kernels referenced by this meta-kernel are as follows: File name Contents --------- -------- naif0009.tls Leapseconds cpck05Mar2004.tpc Satellite orientation and radii 981005_PLTEPH-DE405S.bsp Planetary ephemeris 020514_SE_SAT105.bsp Satellite ephemeris 030201AP_SK_SM546_T45.bsp Spacecraft ephemeris cas_v37.tf Cassini FK 04135_04171pc_psiv2.bc Cassini bus CK cas00084.tsc Cassini SCLK kernel cas_iss_v09.ti Cassini IK \begindata KERNELS_TO_LOAD = ( 'naif0009.tls', 'cpck05Mar2004.tpc', '981005_PLTEPH-DE405S.bsp', '020514_SE_SAT105.bsp', '030201AP_SK_SM546_T45.bsp', 'cas_v37.tf', '04135_04171pc_psiv2.bc', 'cas00084.tsc', 'cas_iss_v09.ti' ) \begintext Example code begins here. #include <stdio.h> #include "SpiceUsr.h" #include "SpiceZmc.h" int main() { /. PROGRAM EX1 ./ /. Local constants ./ #define META "gftfov_ex1.tm" #define TIMFMT "YYYY-MON-DD HR:MN:SC.######::TDB (TDB)" #define TIMLEN 41 #define MAXWIN 10000 /. Local variables ./ SPICEDOUBLE_CELL ( cnfine, MAXWIN ); SPICEDOUBLE_CELL ( result, MAXWIN ); SpiceChar * abcorr; SpiceChar * inst; SpiceChar * obsrvr; SpiceChar * target; SpiceChar * tframe; SpiceChar timstr [2][ TIMLEN ]; SpiceChar * tshape; SpiceDouble endpt [2]; SpiceDouble et0; SpiceDouble et1; SpiceDouble stepsz; SpiceInt i; SpiceInt j; SpiceInt n; /. Load kernels. ./ furnsh_c ( META ); /. Insert search time interval bounds into the confinement window. ./ str2et_c ( "2004 JUN 11 06:30:00 TDB", &et0 ); str2et_c ( "2004 JUN 11 12:00:00 TDB", &et1 ); wninsd_c ( et0, et1, &cnfine ); /. Initialize inputs for the search. ./ inst = "CASSINI_ISS_NAC"; target = "PHOEBE"; tshape = "ELLIPSOID"; tframe = "IAU_PHOEBE"; abcorr = "LT+S"; obsrvr = "CASSINI"; stepsz = 10.0; printf ( "\n" " Instrument: %s\n" " Target: %s\n" "\n", inst, target ); /. Perform the search. ./ ## Restrictions1) The reference frame associated with `inst' must be centered at the observer or must be inertial. No check is done to ensure this. 2) The kernel files to be used by ## Literature_ReferencesNone. ## Author_and_InstitutionN.J. Bachman (JPL) L.S. Elson (JPL) E.D. Wright (JPL) ## Version-CSPICE Version 1.0.0, 15-APR-2009 (NJB) (LSE) (EDW) ## Index_EntriesGF target in instrument FOV search |

Wed Apr 5 17:54:36 2017