Log in

Relevant bibliographies by topics / Reorientation maneuver

Contents

Journal articles

Academic literature on the topic 'Reorientation maneuver'

Author: Grafiati

Published: 22 February 2023

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Reorientation maneuver.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Reorientation maneuver"

1

Kim, Donghoon, James D. Turner, and Henzeh Leeghim. "Reorientation of Asymmetric Rigid Body Using Two Controls." Mathematical Problems in Engineering 2013 (2013): 1–8. http://dx.doi.org/10.1155/2013/708935.

Full text

Abstract:

Most spacecrafts are designed to be maneuvered to achieve pointing goals. This is accomplished usually by designing a three-axis control system, which can achieve arbitrary maneuvers, where the goal is to repoint the spacecraft and match a desired angular velocity at the end of the maneuver. New control laws are required, however, if one of the three-axis control actuators fails. This paper explores suboptimal maneuver strategies when only two control torque inputs are available. To handle this underactuated system control problem, the three-axis maneuver strategy is transformed to two success

APA, Harvard, Vancouver, ISO, and other styles

2

Rahn, Christopher D., and Peter M. Barba. "Reorientation maneuver for spinning spacecraft." Journal of Guidance, Control, and Dynamics 14, no. 4 (1991): 724–28. http://dx.doi.org/10.2514/3.20705.

Full text

APA, Harvard, Vancouver, ISO, and other styles

3

Posani, Massimo, Mauro Pontani, and Paolo Gasbarri. "Nonlinear Slewing Control of a Large Flexible Spacecraft Using Reaction Wheels." Aerospace 9, no. 5 (2022): 244. http://dx.doi.org/10.3390/aerospace9050244.

Full text

Abstract:

Reorientation maneuvers represent a key task for large satellites. This work considers a space vehicle with solar panels and reaction wheels as actuation devices. Solar panels are modeled as flexural beams, using the modal decomposition technique. An inertia-free nonlinear attitude control algorithm, which enjoys quasi-global stability properties, is employed for the numerical simulation of a large reorientation maneuver. Preliminary analysis with ideal actuation allows sizing the control system and identifying the expected elastic displacements. Then, the actuation dynamics is included, and t

APA, Harvard, Vancouver, ISO, and other styles

4

Posani, Massimo, Mauro Pontani, and Paolo Gasbarri. "Nonlinear Slewing Control of a Large Flexible Spacecraft Using Reaction Wheels." Aerospace 9, no. 5 (2022): 244. http://dx.doi.org/10.3390/aerospace9050244.

Full text

Abstract:

Reorientation maneuvers represent a key task for large satellites. This work considers a space vehicle with solar panels and reaction wheels as actuation devices. Solar panels are modeled as flexural beams, using the modal decomposition technique. An inertia-free nonlinear attitude control algorithm, which enjoys quasi-global stability properties, is employed for the numerical simulation of a large reorientation maneuver. Preliminary analysis with ideal actuation allows sizing the control system and identifying the expected elastic displacements. Then, the actuation dynamics is included, and t

APA, Harvard, Vancouver, ISO, and other styles

5

Bang, Hyochoong, Jong-Ah Kim, and Myungsuk Kim. "Optimal Reorientation Maneuver of Bias Momentum Spacecraft." Journal of Guidance, Control, and Dynamics 20, no. 6 (1997): 1076–82. http://dx.doi.org/10.2514/2.4188.

Full text

APA, Harvard, Vancouver, ISO, and other styles

6

Levskii, M. V. "Analytical Solving the Optimal Control Problem of Spacecraft’s Slew Maneuver with Minimal Energy of Rotation." Mekhatronika, Avtomatizatsiya, Upravlenie 21, no. 3 (2020): 174–83. http://dx.doi.org/10.17587/mau.21.174-183.

Full text

Abstract:

Dynamic problem of optimal reorientation from an arbitrary initial attitude into the given final angular position with restricted control which minimizes kinetic energy of spacecraft rotation was solved. Termination time of maneuver is known. Quadratic criterion of quality is applied for finding the optimal control program. Use of integral index in special form concerning angular velocity has helped solve the formulated problem by analytical way. Control law was written down in explicit form. Designing the optimal control is based on quaternion variables and models. It is shown that during opt

APA, Harvard, Vancouver, ISO, and other styles

7

Quinn, Daniel, Daniel Kress, Eric Chang, Andrea Stein, Michal Wegrzynski, and David Lentink. "How lovebirds maneuver through lateral gusts with minimal visual information." Proceedings of the National Academy of Sciences 116, no. 30 (2019): 15033–41. http://dx.doi.org/10.1073/pnas.1903422116.

Full text

Abstract:

Flying birds maneuver effectively through lateral gusts, even when gust speeds are as high as flight speeds. What information birds use to sense gusts and how they compensate is largely unknown. We found that lovebirds can maneuver through 45° lateral gusts similarly well in forest-, lake-, and cave-like visual environments. Despite being diurnal and raised in captivity, the birds fly to their goal perch with only a dim point light source as a beacon, showing that they do not need optic flow or a visual horizon to maneuver. To accomplish this feat, lovebirds primarily yaw their bodies into the

APA, Harvard, Vancouver, ISO, and other styles

8

Gorinevsky, Dimitry, and George Vukovich. "Nonlinear Input Shaping Control of Flexible Spacecraft Reorientation Maneuver." Journal of Guidance, Control, and Dynamics 21, no. 2 (1998): 264–70. http://dx.doi.org/10.2514/2.4252.

Full text

APA, Harvard, Vancouver, ISO, and other styles

9

Urakubo, Takateru, Kazuo Tsuchiya, and Yukio Tada. "REORIENTATION MANEUVER OF A SPACECRAFT COMPOSED OF TWO RIGID BODIES." Proceedings of the International Conference on Motion and Vibration Control 6.1 (2002): 355–60. http://dx.doi.org/10.1299/jsmeintmovic.6.1.355.

Full text

APA, Harvard, Vancouver, ISO, and other styles

10

Endo, Tatsuya, and Seiya Ueno. "OPTIMAL REORIENTATION MANEUVER OF SATELLITES BY TWO REACTION WHEELS WITH ATTITUDE CONSTRAINTS." Proceedings of the International Conference on Motion and Vibration Control 6.2 (2002): 961–66. http://dx.doi.org/10.1299/jsmeintmovic.6.2.961.

Full text

APA, Harvard, Vancouver, ISO, and other styles

More sources

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!