Skip to content
GitLab
Menu
Projects
Groups
Snippets
/
Help
Help
Support
Community forum
Keyboard shortcuts
?
Submit feedback
Contribute to GitLab
Sign in
Toggle navigation
Menu
Open sidebar
Orekit
Orekit
Commits
018bf6fd
Commit
018bf6fd
authored
Feb 06, 2020
by
Bryan Cazabonne
Browse files
Fixed JavaDoc warnings.
parent
e8171b97
Pipeline
#196
passed with stage
in 19 minutes and 19 seconds
Changes
11
Pipelines
2
Hide whitespace changes
Inline
Side-by-side
src/main/java/org/orekit/estimation/measurements/gnss/GRAPHICCombination.java
View file @
018bf6fd
...
...
@@ -25,14 +25,14 @@ import org.orekit.gnss.SatelliteSystem;
* combination of measurements.
* </p>
* <pre>
* m
<sub>f</sub> = 0.5 * (Φ<sub>f</sub> + R<sub>f</sub>
)
* m
f = 0.5 * (Φf + Rf
)
* </pre>
* With:
* <ul>
* <li>m
<sub>f</sub>
: GRAPHIC measurement.</li>
* <li>Φ
<sub>f</sub>
: Phase measurement.</li>
* <li>R
<sub>f</sub>
: Code measurement.</li>
* <li>f
: Frequency.</li>
* <li>m
f
: GRAPHIC measurement.</li>
* <li>Φ
f
: Phase measurement.</li>
* <li>R
f
: Code measurement.</li>
* <li>f : Frequency.</li>
* </ul>
* @author Bryan Cazabonne
* @since 10.1
...
...
src/main/java/org/orekit/estimation/measurements/gnss/MelbourneWubbenaCombination.java
View file @
018bf6fd
...
...
@@ -35,18 +35,18 @@ import org.orekit.gnss.SatelliteSystem;
* narrow-lane combination of code measurements.
* </p>
* <pre>
* m
<sub>MW</sub> = Φ<sub>WL</sub> - R<sub>NL</sub>
* m
<sub>MW</sub> = λ<sub>WL</sub> * N<sub>WL</sub>
+ b + ε
* m
MW = ΦWL- RNL
* m
MW = λWL * NWL
+ b + ε
* </pre>
* With:
* <ul>
* <li>m
<sub>MW</sub>
: Melbourne-Wübbena measurement.</li>
* <li>Φ
<sub>WL</sub>
: Wide-Lane phase measurement.</li>
* <li>R
<sub>NL</sub>
: Narrow-Lane code measurement.</li>
* <li>λ
<sub>WL</sub>
: Wide-Lane wavelength.</li>
* <li>N
<sub>WL</sub>
: Wide-Lane ambiguity (N
<sub>f1</sub> - N<sub>f2</sub>
).</li>
* <li>b
: Satellite and receiver instrumental delays.</li>
* <li>ε
: Measurement noise.</li>
* <li>m
MW
: Melbourne-Wübbena measurement.</li>
* <li>Φ
WL
: Wide-Lane phase measurement.</li>
* <li>R
NL
: Narrow-Lane code measurement.</li>
* <li>λ
WL
: Wide-Lane wavelength.</li>
* <li>N
WL
: Wide-Lane ambiguity (N
f1 - Nf2
).</li>
* <li>b : Satellite and receiver instrumental delays.</li>
* <li>ε : Measurement noise.</li>
* </ul>
* <p>
* {@link NarrowLaneCombination Narrow-Lane} and {@link WideLaneCombination Wide-Lane}
...
...
src/main/java/org/orekit/estimation/measurements/gnss/PhaseMinusCodeCombination.java
View file @
018bf6fd
...
...
@@ -25,14 +25,14 @@ import org.orekit.gnss.SatelliteSystem;
* measurements that can be used for cycle-slip detection.
* </p>
* <pre>
* m
<sub>f</sub> = Φ<sub>f</sub> - R<sub>f</sub>
* m
f = Φf - Rf
* </pre>
* With:
* <ul>
* <li>m
<sub>f</sub>
: Phase minus Code measurement.</li>
* <li>Φ
<sub>f</sub>
: Phase measurement.</li>
* <li>R
<sub>f</sub>
: Code measurement.</li>
* <li>f
: Frequency.</li>
* <li>m
f
: Phase minus Code measurement.</li>
* <li>Φ
f
: Phase measurement.</li>
* <li>R
f
: Code measurement.</li>
* <li>f : Frequency.</li>
* </ul>
* @author Bryan Cazabonne
* @since 10.1
...
...
src/main/java/org/orekit/propagation/FieldSpacecraftState.java
View file @
018bf6fd
...
...
@@ -507,13 +507,13 @@ public class FieldSpacecraftState <T extends RealFieldElement<T>>
* </p>
* <table border="1" cellpadding="5">
* <caption>Extrapolation Error</caption>
* <tr
bg
color
="
#ccccff"><th>interpolation time (s)</th>
* <tr
style="background-
color
:
#ccccff
;
"><th>interpolation time (s)</th>
* <th>position error without derivatives (m)</th><th>position error with derivatives (m)</th></tr>
* <tr><td
bg
color
="
#eeeeff"> 60</td><td> 18</td><td> 1.1</td></tr>
* <tr><td
bg
color
="
#eeeeff">120</td><td> 72</td><td> 9.1</td></tr>
* <tr><td
bg
color
="
#eeeeff">300</td><td> 447</td><td> 140</td></tr>
* <tr><td
bg
color
="
#eeeeff">600</td><td>1601</td><td>1067</td></tr>
* <tr><td
bg
color
="
#eeeeff">900</td><td>3141</td><td>3307</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
"> 60</td><td> 18</td><td> 1.1</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">120</td><td> 72</td><td> 9.1</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">300</td><td> 447</td><td> 140</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">600</td><td>1601</td><td>1067</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">900</td><td>3141</td><td>3307</td></tr>
* </table>
* @param dt time shift in seconds
* @return a new state, shifted with respect to the instance (which is immutable)
...
...
@@ -548,13 +548,13 @@ public class FieldSpacecraftState <T extends RealFieldElement<T>>
* </p>
* <table border="1" cellpadding="5">
* <caption>Extrapolation Error</caption>
* <tr
bg
color
="
#ccccff"><th>interpolation time (s)</th>
* <tr
style="background-
color
:
#ccccff
;
"><th>interpolation time (s)</th>
* <th>position error without derivatives (m)</th><th>position error with derivatives (m)</th></tr>
* <tr><td
bg
color
="
#eeeeff"> 60</td><td> 18</td><td> 1.1</td></tr>
* <tr><td
bg
color
="
#eeeeff">120</td><td> 72</td><td> 9.1</td></tr>
* <tr><td
bg
color
="
#eeeeff">300</td><td> 447</td><td> 140</td></tr>
* <tr><td
bg
color
="
#eeeeff">600</td><td>1601</td><td>1067</td></tr>
* <tr><td
bg
color
="
#eeeeff">900</td><td>3141</td><td>3307</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
"> 60</td><td> 18</td><td> 1.1</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">120</td><td> 72</td><td> 9.1</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">300</td><td> 447</td><td> 140</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">600</td><td>1601</td><td>1067</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">900</td><td>3141</td><td>3307</td></tr>
* </table>
* @param dt time shift in seconds
* @return a new state, shifted with respect to the instance (which is immutable)
...
...
src/main/java/org/orekit/propagation/SpacecraftState.java
View file @
018bf6fd
...
...
@@ -423,13 +423,13 @@ public class SpacecraftState
* </p>
* <table border="1" cellpadding="5">
* <caption>Extrapolation Error</caption>
* <tr
bg
color
="
#ccccff"><th>interpolation time (s)</th>
* <tr
style="background-
color
:
#ccccff
;
"><th>interpolation time (s)</th>
* <th>position error without derivatives (m)</th><th>position error with derivatives (m)</th></tr>
* <tr><td
bg
color
="
#eeeeff"> 60</td><td> 18</td><td> 1.1</td></tr>
* <tr><td
bg
color
="
#eeeeff">120</td><td> 72</td><td> 9.1</td></tr>
* <tr><td
bg
color
="
#eeeeff">300</td><td> 447</td><td> 140</td></tr>
* <tr><td
bg
color
="
#eeeeff">600</td><td>1601</td><td>1067</td></tr>
* <tr><td
bg
color
="
#eeeeff">900</td><td>3141</td><td>3307</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
"> 60</td><td> 18</td><td> 1.1</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">120</td><td> 72</td><td> 9.1</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">300</td><td> 447</td><td> 140</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">600</td><td>1601</td><td>1067</td></tr>
* <tr><td
style="background-
color
:
#eeeeff
;
">900</td><td>3141</td><td>3307</td></tr>
* </table>
* @param dt time shift in seconds
* @return a new state, shifted with respect to the instance (which is immutable)
...
...
src/main/java/org/orekit/propagation/analytical/gnss/BeidouPropagator.java
View file @
018bf6fd
...
...
@@ -84,13 +84,14 @@ public class BeidouPropagator extends AbstractGNSSPropagator {
* </p>
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
* Another data context can be set using
* {@code Builder(final BeidouOrbitalElements gpsOrbElt, final Frames frames)}</p>
*
* @param bdsOrbElt the Beidou orbital elements to be used by the Beidou propagator.
* @see #attitudeProvider(AttitudeProvider provider)
* @see #mass(double mass)
* @see #eci(Frame inertial)
* @see #ecef(Frame bodyFixed)
* @see #BeidouPropagator.Builder(BeidouOrbitalElements bdsOrbElt, Frames frames)
*/
@DefaultDataContext
public
Builder
(
final
BeidouOrbitalElements
bdsOrbElt
)
{
...
...
src/main/java/org/orekit/propagation/analytical/gnss/GLONASSAnalyticalPropagator.java
View file @
018bf6fd
...
...
@@ -156,13 +156,14 @@ public class GLONASSAnalyticalPropagator extends AbstractAnalyticalPropagator {
* </p>
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
* Another data context can be set using
* {@code Builder(final GLONASSOrbitalElements gpsOrbElt, final DataContext dataContext)}</p>
*
* @param glonassOrbElt the GLONASS orbital elements to be used by the GLONASS propagator.
* @see #attitudeProvider(AttitudeProvider provider)
* @see #mass(double mass)
* @see #eci(Frame inertial)
* @see #ecef(Frame bodyFixed)
* @see #GLONASSAnalyticalPropagator.Builder(GLONASSOrbitalElements glonassOrbElt, DataContext dataContext)
*/
@DefaultDataContext
public
Builder
(
final
GLONASSOrbitalElements
glonassOrbElt
)
{
...
...
src/main/java/org/orekit/propagation/analytical/gnss/GPSPropagator.java
View file @
018bf6fd
...
...
@@ -82,13 +82,14 @@ public class GPSPropagator extends AbstractGNSSPropagator {
* </p>
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
* Another data context can be set using
* {@code Builder(final GPSOrbitalElements gpsOrbElt, final Frames frames)}</p>
*
* @param gpsOrbElt the GPS orbital elements to be used by the GPSpropagator.
* @see #attitudeProvider(AttitudeProvider provider)
* @see #mass(double mass)
* @see #eci(Frame inertial)
* @see #ecef(Frame bodyFixed)
* @see #GPSPropagator.Builder(GPSOrbitalElements gpsOrbElt, Frames frames)
*/
@DefaultDataContext
public
Builder
(
final
GPSOrbitalElements
gpsOrbElt
)
{
...
...
src/main/java/org/orekit/propagation/analytical/gnss/GalileoPropagator.java
View file @
018bf6fd
...
...
@@ -83,13 +83,14 @@ public class GalileoPropagator extends AbstractGNSSPropagator {
* </p>
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
* Another data context can be set using
* {@code Builder(final GalileoOrbitalElements gpsOrbElt, final Frames frames)}</p>
*
* @param galileoOrbElt the Galileo orbital elements to be used by the Galileo propagator.
* @see #attitudeProvider(AttitudeProvider provider)
* @see #mass(double mass)
* @see #eci(Frame inertial)
* @see #ecef(Frame bodyFixed)
* @see #GalileoPropagator.Builder(GalileoOrbitalElements galileoOrbElt, Frames frames)
*/
@DefaultDataContext
public
Builder
(
final
GalileoOrbitalElements
galileoOrbElt
)
{
...
...
src/main/java/org/orekit/propagation/analytical/gnss/QZSSPropagator.java
View file @
018bf6fd
...
...
@@ -85,13 +85,14 @@ public class QZSSPropagator extends AbstractGNSSPropagator {
* </p>
*
* <p>This constructor uses the {@link DataContext#getDefault() default data context}.
* Another data context can be set using
* {@code Builder(final QZSSOrbitalElements gpsOrbElt, final Frames frames)}</p>
*
* @param qzssOrbElt the QZSS orbital elements to be used by the QZSSpropagator.
* @see #attitudeProvider(AttitudeProvider provider)
* @see #mass(double mass)
* @see #eci(Frame inertial)
* @see #ecef(Frame bodyFixed)
* @see #QZSSPropagator.Builder(QZSSOrbitalElements qzssOrbElt, Frames frames)
*/
@DefaultDataContext
public
Builder
(
final
QZSSOrbitalElements
qzssOrbElt
)
{
...
...
src/main/java/org/orekit/propagation/events/AbstractDetector.java
View file @
018bf6fd
...
...
@@ -33,7 +33,7 @@ public abstract class AbstractDetector<T extends AbstractDetector<T>> implements
/** Default convergence threshold (s). */
public
static
final
double
DEFAULT_THRESHOLD
=
1
.
e
-
6
;
/** Default
c
maximum number of iterations in the event time search. */
/** Default maximum number of iterations in the event time search. */
public
static
final
int
DEFAULT_MAX_ITER
=
100
;
/** Max check interval. */
...
...
Write
Preview
Supports
Markdown
0%
Try again
or
attach a new file
.
Attach a file
Cancel
You are about to add
0
people
to the discussion. Proceed with caution.
Finish editing this message first!
Cancel
Please
register
or
sign in
to comment