Maneuvers - Historique des versions

Admin : /* Impulsive maneuver */

2019-11-08T10:01:46Z

Impulsive maneuver

← Version précédente		Version du 8 novembre 2019 à 10:01
Ligne 21 :		Ligne 21 :
	*** The frame in which the maneuver is defined		*** The frame in which the maneuver is defined
	*** The maneuver components (Cartesian coordinates or a norm and two angles)		*** The maneuver components (Cartesian coordinates or a norm and two angles)

	** if it is by orbital increments:		** if it is by orbital increments:
	*** on semi-major axis		*** on semi-major axis

Admin : /* Impulsive maneuver */

2019-11-08T10:01:33Z

Impulsive maneuver

← Version précédente		Version du 8 novembre 2019 à 10:01
Ligne 21 :		Ligne 21 :
	*** The frame in which the maneuver is defined		*** The frame in which the maneuver is defined
	*** The maneuver components (Cartesian coordinates or a norm and two angles)		*** The maneuver components (Cartesian coordinates or a norm and two angles)

			** if it is by orbital increments:
			*** on semi-major axis
			*** on eccentricity (and semi-major axis eventually)
			*** on inclination (and semi-major axis eventually)

	[[Fichier:ImpulseManeuverCoordinates.png]]		[[Fichier:ImpulseManeuverCoordinates.png]]
Ligne 31 :		Ligne 36 :
	\end{cases}		\end{cases}
	</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]		</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]
	** if it is by orbital increments:
	*** on semi-major axis
	*** on eccentricity (and semi-major axis eventually)
	*** on inclination (and semi-major axis eventually)

	* The orbital event that will trigger the maneuver (<font color=#FF0000>''be careful that the orbital event is not indefinite as AOL when inclination is equal to zero''</font>)		* The orbital event that will trigger the maneuver (<font color=#FF0000>''be careful that the orbital event is not indefinite as AOL when inclination is equal to zero''</font>)

Admin : /* Impulsive maneuver */

2019-11-08T10:00:38Z

Impulsive maneuver

← Version précédente		Version du 8 novembre 2019 à 10:00
Ligne 31 :		Ligne 31 :
	\end{cases}		\end{cases}
	</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]		</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]


	** if it is by orbital increments:		** if it is by orbital increments:
	*** on semi-major axis		*** on semi-major axis

Admin : /* Impulsive maneuver */

2019-11-08T10:00:19Z

Impulsive maneuver

← Version précédente		Version du 8 novembre 2019 à 10:00
Ligne 17 :		Ligne 17 :
	The user will have to define:		The user will have to define:
	* The name of the maneuver		* The name of the maneuver
	* Since V2.1, the type of maneuver (standard or by orbital increment)		* Since V11.4, the type of maneuver (standard or by orbital increment)
	** if standard type is chosen, we will have to give:		** if standard type is chosen, we will have to give:
	*** The frame in which the maneuver is defined		*** The frame in which the maneuver is defined
Ligne 31 :		Ligne 31 :
	\end{cases}		\end{cases}
	</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]		</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]


	** if it is by orbital increments:		** if it is by orbital increments:

Admin : /* Impulsive maneuver */

2019-11-08T09:59:16Z

Impulsive maneuver

← Version précédente		Version du 8 novembre 2019 à 09:59
Ligne 17 :		Ligne 17 :
	The user will have to define:		The user will have to define:
	* The name of the maneuver		* The name of the maneuver
	* The frame in which the maneuver is defined		* Since V2.1, the type of maneuver (standard or by orbital increment)
	* The maneuver components (Cartesian coordinates or a norm and two angles)		** if standard type is chosen, we will have to give:
			*** The frame in which the maneuver is defined
			*** The maneuver components (Cartesian coordinates or a norm and two angles)

	[[Fichier:ImpulseManeuverCoordinates.png]]		[[Fichier:ImpulseManeuverCoordinates.png]]
Ligne 29 :		Ligne 31 :
	\end{cases}		\end{cases}
	</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]		</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]

			** if it is by orbital increments:
			*** on semi-major axis
			*** on eccentricity (and semi-major axis eventually)
			*** on inclination (and semi-major axis eventually)

	* The orbital event that will trigger the maneuver (<font color=#FF0000>''be careful that the orbital event is not indefinite as AOL when inclination is equal to zero''</font>)		* The orbital event that will trigger the maneuver (<font color=#FF0000>''be careful that the orbital event is not indefinite as AOL when inclination is equal to zero''</font>)

Admin : /* Impulsive maneuver */

2018-10-18T14:17:10Z

Impulsive maneuver

← Version précédente		Version du 18 octobre 2018 à 14:17
Ligne 20 :		Ligne 20 :
	* The maneuver components (Cartesian coordinates or a norm and two angles)		* The maneuver components (Cartesian coordinates or a norm and two angles)

	[[Fichier:~~ImpulseManeuverCartesian~~.png]]		[[Fichier:ImpulseManeuverCoordinates.png]]
	The components and the angles are related by:		The components and the angles are related by:
	<math>		<math>

Admin : /* Impulsive maneuver */

2018-10-18T14:15:50Z

Impulsive maneuver

← Version précédente		Version du 18 octobre 2018 à 14:15
Ligne 20 :		Ligne 20 :
	* The maneuver components (Cartesian coordinates or a norm and two angles)		* The maneuver components (Cartesian coordinates or a norm and two angles)

			[[Fichier:ImpulseManeuverCartesian.png]]
	The components and the angles are related by:		The components and the angles are related by:
	<math>		<math>

Admin : /* Impulsive maneuver */

2018-10-18T14:13:51Z

Impulsive maneuver

← Version précédente		Version du 18 octobre 2018 à 14:13
Ligne 20 :		Ligne 20 :
	* The maneuver components (Cartesian coordinates or a norm and two angles)		* The maneuver components (Cartesian coordinates or a norm and two angles)

	The components and the angles are related by:		The components and the angles are related by:
	<math>		<math>
	\begin{cases}		\begin{cases}

Admin : /* Impulsive maneuver */

2018-10-18T14:13:41Z

Impulsive maneuver

← Version précédente		Version du 18 octobre 2018 à 14:13
Ligne 20 :		Ligne 20 :
	* The maneuver components (Cartesian coordinates or a norm and two angles)		* The maneuver components (Cartesian coordinates or a norm and two angles)

	The components and the angles are related by:		The components and the angles are related by:
	<math>		<math>
	\begin{cases}		\begin{cases}
Ligne 27 :		Ligne 27 :
	ΔV_z = \\|\overrightarrow{ΔV}\\|\ sin(β)		ΔV_z = \\|\overrightarrow{ΔV}\\|\ sin(β)
	\end{cases}		\end{cases}
	</math>		</math> where α ∈ [0,2π] and β ∈ [-π/2,π/2]

	where α ∈ [0,2π] and β ∈ [-π/2,π/2]

	* The orbital event that will trigger the maneuver (<font color=#FF0000>''be careful that the orbital event is not indefinite as AOL when inclination is equal to zero''</font>)		* The orbital event that will trigger the maneuver (<font color=#FF0000>''be careful that the orbital event is not indefinite as AOL when inclination is equal to zero''</font>)

Admin : /* Impulsive maneuver */

2018-10-18T14:13:06Z

Impulsive maneuver

← Version précédente		Version du 18 octobre 2018 à 14:13
Ligne 19 :		Ligne 19 :
	* The frame in which the maneuver is defined		* The frame in which the maneuver is defined
	* The maneuver components (Cartesian coordinates or a norm and two angles)		* The maneuver components (Cartesian coordinates or a norm and two angles)
	~~[[Fichier:ImpulseManeuverCoordinates.png]] [[Fichier:ImpulseManeuverDirection.png]]~~

	The components and the angles are related by:		The components and the angles are related by:

Maneuvers - Historique des versions

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */

Admin : /* Impulsive maneuver */