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Task scheduling method with quantity first

A task scheduling and task technology, which is applied in the direction of program startup/switching, multi-channel program installation, etc., can solve the problem of inability to meet the needs of fast attitude maneuver imaging satellite task scheduling, the inapplicability of fast attitude maneuver imaging satellites, and conflict identification and resolution rules. Trouble and other problems, to achieve the effect of fast calculation, resolve conflict judgments and trade-offs, and avoid wasting time

Active Publication Date: 2013-07-24
AEROSPACE DONGFANGHONG SATELLITE
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of this method is that due to the complexity of the constraints, the problem scale is large, the solution is difficult and time-consuming
For example, in the ASPEN system, due to the troublesome conflict identification and resolution rules adopted, the solution efficiency is low. In the application of EO-1, only 4 tasks can be scheduled every day, which is difficult to meet the requirements of multi-task scheduling;
[0009] Third, most of the existing scheduling methods are related to the specific application satellites, and the design of the model is closely related to the specific spaceborne equipment, which is not general and universal
Traditional scheduling methods are not suitable for fast attitude maneuvering imaging satellites, and cannot meet the needs of task scheduling for fast attitude maneuvering imaging satellites

Method used

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  • Task scheduling method with quantity first

Examples

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Embodiment

[0127] Consider a fast attitude maneuvering imaging satellite operating in a sun-synchronous circular orbit. At 00:00:00.000 UTC on July 26, 2009, the instantaneous root number is 7051.2km, the orbital inclination is 97.3087°, and the right ascension of the ascending node is 249.758°, latitude argument 0°. The satellite attitude maneuver range is ±45° in the pitch direction and roll direction, and the attitude control capabilities are 0° / 15s, 15° / 25s, 30° / 35s, 45° / 45s.

[0128] The geographic latitude and longitude information of the target is shown in Table 1, and the longitude and latitude of the four vertices of each target correspond one by one in order.

[0129] Table 1 Target geographic longitude and latitude

[0130]

[0131] The steps of the quantity-first task scheduling method are as follows:

[0132] (1) Task area strip division

[0133] According to the camera width, the longitude and latitude of the mission area, and the satellite sub-satellite point, the mi...

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Abstract

The invention discloses a task scheduling method with quantity first. The task scheduling method comprises the following steps of: (1) dividing a task region into stripes; (2) calculating a visible time interval of a satellite for each stripe and sequencing according to starting moments of visible time windows so as to acquire a task sequence; (3) calculating an observation lasting time of each task stripe in the task sequence by adopting a secant method; (4) processing tasks in the task sequence in order, judging whether the current task and the last arranged task are conflicted with each other according to an attitude maneuver time of the satellite, if so, not arranging the current task, otherwise, stepping into a step (5); and (5) acquiring a foresight task group of the current task, judging whether the current task and tasks in the foresight task group are conflicted with one another, if not, arranging the current task, otherwise, accepting or rejecting the current task, and if the current task is retained, writing the current task into a satellite motion sequence and taking the current task as a result of the task scheduling.

Description

technical field [0001] The invention belongs to the field of satellite task planning and scheduling, and relates to a satellite task scheduling method. Background technique [0002] Rapid attitude maneuvering imaging satellites can realize a variety of complex imaging modes with the help of rapid attitude maneuvering capabilities. Compared with traditional earth observation satellites that use sub-satellite point imaging, the rapid attitude maneuver capability greatly increases the satellite's observation opportunities for targets, and thus has stronger observation capabilities. Each imaging mode of the rapid attitude maneuvering imaging satellite is accompanied by multiple operations such as attitude maneuvering, camera switching on and off, and these operations form a coherent control command sequence. Due to the large number of instructions, the reliability of instruction arrangement and annotation and the real-time execution of instructions cannot be guaranteed. Therefo...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F9/48G06F9/46
Inventor 王抒雁杨芳阎诚赵键谢松姚锋廉振宇
Owner AEROSPACE DONGFANGHONG SATELLITE
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