Control law design for the energy management phase of a winged re-entry vehicle

Taro Tsukamoto; Masaaki Yanagihara; Yoshikazu Miyazawa; Hitoshi Takatsuka

Control law design for the energy management phase of a winged re-entry vehicle

Taro Tsukamoto, Masaaki Yanagihara, Yoshikazu Miyazawa, Hitoshi Takatsuka

Flight Dynamics Lab

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

1 Citation (Scopus)

Abstract

A control law for the terminal area energy management (TAEM) phase of a winged re-entry vehicle was designed. During the TAEM phase, the dynamics of the vehicle vary considerably because of changes of velocity and altitude. In addition, there is a significant error in the measured value of Mach number, which is used as a scheduling parameter. The multiple delay model and multiple design point (MDM/MDP) approach is a practical method of designing a controller that can operate over a large range of flight conditions. In this paper, the MDM/MDP approach is used to design a gain-scheduled controller and the resulting design is verified by linear stability analysis, linear command response, and nonlinear flight simulation.

Original language	English
Title of host publication	Guidance, Navigation, and Control Conference and Exhibit
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
Pages	593-598
Number of pages	6
Publication status	Published - 1999
Event	Guidance, Navigation, and Control Conference and Exhibit, 1999 - Portland, United States Duration: Aug 9 1999 → Aug 11 1999

Other

Other	Guidance, Navigation, and Control Conference and Exhibit, 1999
Country/Territory	United States
City	Portland
Period	8/9/99 → 8/11/99

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Control and Systems Engineering
Electrical and Electronic Engineering

Cite this

Control law design for the energy management phase of a winged re-entry vehicle. / Tsukamoto, Taro; Yanagihara, Masaaki; Miyazawa, Yoshikazu et al.
Guidance, Navigation, and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 1999. p. 593-598.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Tsukamoto, T, Yanagihara, M, Miyazawa, Y & Takatsuka, H 1999, Control law design for the energy management phase of a winged re-entry vehicle. in Guidance, Navigation, and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, pp. 593-598, Guidance, Navigation, and Control Conference and Exhibit, 1999, Portland, United States, 8/9/99.

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AB - A control law for the terminal area energy management (TAEM) phase of a winged re-entry vehicle was designed. During the TAEM phase, the dynamics of the vehicle vary considerably because of changes of velocity and altitude. In addition, there is a significant error in the measured value of Mach number, which is used as a scheduling parameter. The multiple delay model and multiple design point (MDM/MDP) approach is a practical method of designing a controller that can operate over a large range of flight conditions. In this paper, the MDM/MDP approach is used to design a gain-scheduled controller and the resulting design is verified by linear stability analysis, linear command response, and nonlinear flight simulation.

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BT - Guidance, Navigation, and Control Conference and Exhibit

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T2 - Guidance, Navigation, and Control Conference and Exhibit, 1999

Y2 - 9 August 1999 through 11 August 1999

ER -

Control law design for the energy management phase of a winged re-entry vehicle

Abstract

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All Science Journal Classification (ASJC) codes

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