期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2021; 68 (3)
High-inclination near-circular orbits are valuable for Europa's global observation. However, the eccentricity drifts due to Jovian third-body gravity ......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2021; 68 (2)
The electrodynamic tether (EDT) is a type of propulsion system that uses the geomagnetic field and ionospheric plasma and has the potential to conduct......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, ; ()
Thispaper investigates the micro-satellite cluster long-distance gathering control problem including initialization, orbit maintenance and collision a......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2020; 67 (1)
Root locus plots are one of the basic design tools in classical control. They help the designer tune control gains which appear linearly in the coeffi......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2020; 67 (1)
Hypersonic aircrafts are introduced as a platform for cost-efficient access to space. However, challenging problems of control hypersonic aircrafts ex......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2020; 67 (4)
Solving minimum-time low-thrust orbital transfer problems in the three-body problem by indirect methods is an extremely difficult task, which is mainl......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2020; 67 (4)
The typical hovering mission contains three stages: the orbit transfer from the original orbit to the hovering orbit; hovering in the orbit; and the o......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2020; 67 (4)
In recent years there has been an overwhelming demand for the development of the technology of autonomous rendezvous, in which the rapid and accurate ......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2020; 67 (4)
A rapid trajectory optimization method is proposed to solve the fuel-optimal Earth-landing problem of reusable rockets, in which the nonlinear aerodyn......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2019; 66 (4)
To design a free-return orbit for manned lunar mission based on low earth orbit (LEO) rendezvous, an adaptive LEO-phase free-return orbit design metho......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2019; 66 (4)
A methodology for modeling a rotating paraboloidal thin-shell structure attached to a spacecraft body is proposed considering its geometric nonlinear ......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2019; 66 (1)
In this paper, active control of a 6-DOF space robot with flexible panels using singular perturbation method is investigated. Dynamic model of the sys......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2019; 66 (1)
Space debris is increasingly threatening, especially small space debris on the order of centimeters because of the difficulties in detecting and clean......
期刊： JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2019; 66 (3)
In this paper, deployment dynamics of a large-scale flexible solar array system on the ground is investigated. Firstly, the structure of the ground so......
