docbook에서 산소를 사용하여 프로세스를 수행하는 동안 일부를 변경해야합니다.XSLT를 사용하여 para 요소 뒤에 섹션 요소를 닫아야합니다.
내 입력 XML 파일은 다음과 같습니다
으로 사용<section><title>DESCRIPTION</title>
<para>The A380 is available with two types of turbofan engines, the
Rolls-Royce Trent 900 (variants A380-841, −842 and −843F) or the Engine
Alliance GP7000 (A380-861 and −863F). Noise reduction was an important
requirement in the A380 design, and particularly affects engine design.</para>
<section><title>Wing Landing Gear</title>
<section><para>Each wing landing gear has a leg assembly and
a four-wheel bogie beam. The WLG leg includes a Bogie Trim Actuator
(BTA) and an oleo-pneumatic shock absorber.</para>
</section></section><section><title>Body Landing Gear</title>
<section><para>The two body landing gears have a six-wheel bogie
beam and a leg assembly that includes an oleo- pneumatic shock absorber.
A two-piece drag-stay assembly mechanically locks the leg in the extended
position.</para>
</section></section></section>
XSL (2.0) : 내가 갖는
<xsl:template match="*|text()|@*">
<xsl:copy>
<xsl:apply-templates select="@*"/>
<xsl:apply-templates/>
</xsl:copy>
</xsl:template>
<xsl:template match="section">
<section>
<xsl:apply-templates select="node()[not(self::section)]"/>
</section>
<xsl:apply-templates select="section"/>
</xsl:template>
<xsl:template match="section/section[para]">
<xsl:apply-templates/>
</xsl:template>
<xsl:template match="para">
<p>
<xsl:apply-templates/>
</p>
</xsl:template>
출력은 다음과 같습니다
<section>
<title>DESCRIPTION</title>
<p>The A380 is available with two types of turbofan engines, the
Rolls-Royce Trent 900 (variants A380-841, −842 and −843F) or the Engine
Alliance GP7000 (A380-861 and −863F). Noise reduction was an important
requirement in the A380 design, and particularly affects engine design.</p>
</section>
<section>
<title>Wing Landing Gear</title>
</section>
<p>Each wing landing gear has a leg assembly and
a four-wheel bogie beam. The WLG leg includes a Bogie Trim Actuator
(BTA) and an oleo-pneumatic shock absorber.</p>
<section>
<title>Body Landing Gear</title>
</section>
<p>The two body landing gears have a six-wheel bogie
beam and a leg assembly that includes an oleo- pneumatic shock absorber.
A two-piece drag-stay assembly mechanically locks the leg in the extended
position.</p>
예상 출력 XML 요구 :
<section>
<title>DESCRIPTION</title>
<p>The A380 is available with two types of turbofan engines, the
Rolls-Royce Trent 900 (variants A380-841, −842 and −843F) or the Engine
Alliance GP7000 (A380-861 and −863F). Noise reduction was an important
requirement in the A380 design, and particularly affects engine design.</p>
</section>
<section>
<title>Wing Landing Gear</title>
<p>Each wing landing gear has a leg assembly and
a four-wheel bogie beam. The WLG leg includes a Bogie Trim Actuator
(BTA) and an oleo-pneumatic shock absorber.</p></section>
<section>
<title>Body Landing Gear</title>
<p>The two body landing gears have a six-wheel bogie
beam and a leg assembly that includes an oleo- pneumatic shock absorber.
A two-piece drag-stay assembly mechanically locks the leg in the extended
position.</p></section>
코드 및 가이드를 참조하십시오. 사전
[ask] 및 [mcve]를 참조하십시오. – Mat
확인. 감사. 나중에 사용하기 위해 할 것입니다 –