A re-entry guidance law employing simple real-time integration-Reference-Cited by-同舟云学术

A re-entry guidance law employing simple real-time integration

Published:1998-08-10 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation, and Control Conference and Exhibit
language:
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Author:

Ishizuka Koji¹,Shimura Koji²,Ishimoto Shinji³

Affiliation:

1. MHI Aerospace Systems Corp., Nagoya, Japan

2. Mitsubishi Heavy Industries, Ltd., Nagoya, Japan

3. NASDA, Tokyo, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4329

Reference9 articles.

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2. EH: energyheight RN: radius of vehiclenose V: velocity po: density at sea level g: gravity acceleration S: vehiclereference area h: altitude A: constant (=1.1X105) D: dragacceleration m: vehiclemass L: lift acceleration Nz: loadfactor y. flight path angle q : dynamicpressure a: angle ofattack a: bank angle -2000 0 2000 4000 6000 8000

3. Range-lo-<3o [km] 0 1000 2000 3000 4000 5000 6000 7000 8000

4. EarthRelativeVelocity[m/sec] 0 1000 2000 3000 4000 5000 6000 7000 8000

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