The trajectory planning of spacecraft based on optimal quintic polynomial

Yanghua Li; Bo Mo

doi:10.1109/MIC.2013.6758098

The trajectory planning of spacecraft based on optimal quintic polynomial

Yanghua Li, Bo Mo

School of Aerospace Engineering

Beijing Institute of Technology

Research output: Contribution to conference › Paper › peer-review

3 Citations (Scopus)

Abstract

This paper focuses on the implementation and application of the quintic polynomial in the spacecraft trajectory planning. Firstly, the kinematics model and dynamics model of the spacecraft is established. Secondly, the PID control algorithm is used to control the spacecraft. Thirdly, in order to achieve fast and flexible of the spacecraft attitude maneuver, the coefficients of the quintic polynomial are adjusted continuously to optimize the spacecraft. At last, this paper uses Simulink for the simulation, such that the maneuver which is not less than 40 ° is completed within a predetermined period of time angle and such that the attitude angle, attitude angular velocity, and posture angular acceleration can be smoothed.

Original language	English
Pages	865-868
Number of pages	4
DOIs	https://doi.org/10.1109/MIC.2013.6758098
Publication status	Published - 2013
Event	2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013 - Harbin, China Duration: 16 Aug 2013 → 18 Aug 2013

Conference

Conference	2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013
Country/Territory	China
City	Harbin
Period	16/08/13 → 18/08/13

Keywords

Quintic polynomial
Spacecraft attitude
Trajectory planning

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10.1109/MIC.2013.6758098

Cite this

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abstract = "This paper focuses on the implementation and application of the quintic polynomial in the spacecraft trajectory planning. Firstly, the kinematics model and dynamics model of the spacecraft is established. Secondly, the PID control algorithm is used to control the spacecraft. Thirdly, in order to achieve fast and flexible of the spacecraft attitude maneuver, the coefficients of the quintic polynomial are adjusted continuously to optimize the spacecraft. At last, this paper uses Simulink for the simulation, such that the maneuver which is not less than 40 ° is completed within a predetermined period of time angle and such that the attitude angle, attitude angular velocity, and posture angular acceleration can be smoothed.",

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AU - Li, Yanghua

AU - Mo, Bo

PY - 2013

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N2 - This paper focuses on the implementation and application of the quintic polynomial in the spacecraft trajectory planning. Firstly, the kinematics model and dynamics model of the spacecraft is established. Secondly, the PID control algorithm is used to control the spacecraft. Thirdly, in order to achieve fast and flexible of the spacecraft attitude maneuver, the coefficients of the quintic polynomial are adjusted continuously to optimize the spacecraft. At last, this paper uses Simulink for the simulation, such that the maneuver which is not less than 40 ° is completed within a predetermined period of time angle and such that the attitude angle, attitude angular velocity, and posture angular acceleration can be smoothed.

AB - This paper focuses on the implementation and application of the quintic polynomial in the spacecraft trajectory planning. Firstly, the kinematics model and dynamics model of the spacecraft is established. Secondly, the PID control algorithm is used to control the spacecraft. Thirdly, in order to achieve fast and flexible of the spacecraft attitude maneuver, the coefficients of the quintic polynomial are adjusted continuously to optimize the spacecraft. At last, this paper uses Simulink for the simulation, such that the maneuver which is not less than 40 ° is completed within a predetermined period of time angle and such that the attitude angle, attitude angular velocity, and posture angular acceleration can be smoothed.

KW - Quintic polynomial

KW - Spacecraft attitude

KW - Trajectory planning

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T2 - 2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013

Y2 - 16 August 2013 through 18 August 2013

ER -

The trajectory planning of spacecraft based on optimal quintic polynomial

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Keywords

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